阅读说明：本技术 惯性传感装置 (Inertial sensor ) 是由 宋健宇 石仁利 汪滔 于 2014-04-25 设计创作，主要内容包括：提供用于确定可移动物体的空间位置的改进型传感装置。一方面,用于确定可移动物体的空间位置的装置包括：由可移动物体携带的支撑基座；一个或多个加速度计通过第一阻尼元件连接至所述支撑基座,所述第一阻尼元件用于阻尼所述一个或多个加速度计的运动；以及一个或多个陀螺仪通过第二阻尼元件与连接至所述支撑基座,所述第二阻尼元件用于阻尼所述一个或多个陀螺仪的运动,其中由所述第一阻尼元件提供的运动阻尼量大于由所述第二阻尼元件提供的运动阻尼量。(An improved sensing device for determining the spatial position of a movable object is provided. In one aspect, an apparatus for determining a spatial position of a movable object comprises: a support base carried by the movable object; one or more accelerometers connected to the support base by a first damping element for damping movement of the one or more accelerometers; and one or more gyroscopes connected to the support base by a second damping element for damping motion of the one or more gyroscopes, wherein the amount of motion damping provided by the first damping element is greater than the amount of motion damping provided by the second damping element.)

1. An apparatus for determining the spatial position of a movable object, the apparatus comprising:

A support base carried by the movable object;

a first inertial sensor connected to the support base by a first damping element for damping movement of the first inertial sensor; and

A second inertial sensor is connected to the support base by a second damping element for damping movement of the second inertial sensor, wherein the first inertial sensor and the second inertial sensor each comprise a different sensor type, the first damping element and the second damping element having different damping characteristics.

2. The apparatus of claim 1, wherein the first inertial sensor and the second inertial sensor require different amounts of motion damping, and wherein the damping characteristic of the first damping element and the damping characteristic of the second damping element are each configured to provide different amounts of motion damping.

3. The apparatus of claim 2, wherein the first inertial sensor comprises an accelerometer and the second inertial sensor comprises a gyroscope, wherein the damping characteristics of the first damping element and the damping characteristics of the second damping element are configured to provide a greater amount of motion damping to the accelerometer than to the gyroscope.

4. The device of claim 3, wherein the damping characteristics of the first damping element and the second damping element comprise a stiffness of the first damping element and a stiffness of the second damping element, respectively, wherein the stiffness of the first damping element is less than the stiffness of the second damping element.

5. The apparatus of claim 4, wherein the stiffness of the first damping element is configured to reduce noise associated with signals generated by the accelerometer and the stiffness of the second damping element is configured to reduce noise associated with signals generated by the gyroscope.

6. The apparatus of claim 3, wherein the accelerometer comprises a micro-electro-mechanical system (MEMS) accelerometer and the gyroscope comprises a MEMS gyroscope.

7. the device of claim 1, wherein the damping characteristics comprise a stiffness and/or viscoelasticity of the first damping element and the second damping element.

8. The device of claim 7, wherein the damping characteristic comprises a stiffness of the first damping element and the second damping element, wherein the stiffness of the first damping element is less than the stiffness of the second damping element.

9. The device of claim 1, wherein the first and second damping elements each comprise at least one of: a sponge, foam, rubber, gel, piezoelectric material, or shape memory material.

10. The device of claim 1, wherein the first damping element and the second damping element each have an active damping characteristic and/or a passive damping characteristic.

background

In military and civil applications, unmanned vehicles, such as unmanned aerial vehicles, may be used to perform surveillance, reconnaissance, and reconnaissance tasks. Unmanned vehicles may be capable of autonomous navigation or semi-autonomous navigation in an environment. In some cases, the unmanned vehicle may include various sensing devices, such as an Inertial Measurement Unit (IMU), for determining the current spatial position of the unmanned vehicle relative to the surrounding environment.

However, in some cases, the performance of such sensing devices may not be optimal. For example, IMUs and other inertial sensing devices may be susceptible to noise or measurement drift caused by vehicle vibrations. However, the existing strategies for vibration reduction and/or vibration isolation for IMUs and other inertial sensing devices may negatively impact the sensitivity, accuracy, and response time of these devices.

Disclosure of Invention

There is a need for an improved sensing device for determining the spatial position of a movable object. Embodiments disclosed herein provide sensing devices that include one or more accelerometers and one or more gyroscopes for detecting acceleration and rotation, respectively, of a movable object. The accelerometer and gyroscope may be connected to the support base by respective damping elements for providing a predetermined amount of motion damping. In some cases, the amount of motion damping required for optimal accelerometer performance may be different than the amount required for optimal gyroscope performance. Thus, the amount of motion damping applied to the accelerometer and gyroscope may be varied by adjusting the characteristics of the corresponding damping elements. Advantageously, this approach can be used to tailor the damping parameters for each sensor type, thereby reducing the incidence of noise and measurement drift, while maintaining a satisfactory level of sensitivity, accuracy and responsiveness of the sensor.

Accordingly, in one aspect, there is provided an apparatus for determining the spatial position of a movable object, the apparatus comprising:

A support base carried by the movable object;

a first inertial sensor connected to the support base by a first damping element for damping movement of the first inertial sensor; and

A second inertial sensor is connected to the support base by a second damping element for damping movement of the second inertial sensor, wherein the first inertial sensor and the second inertial sensor each comprise a different sensor type, the first damping element and the second damping element having different damping characteristics.

in some embodiments, the first inertial sensor and the second inertial sensor require different amounts of motion damping, and the damping characteristic of the first damping element and the damping characteristic of the second damping element are each used to provide different amounts of motion damping.

In some embodiments, the first inertial sensor comprises an accelerometer and the second inertial sensor comprises a gyroscope, wherein the damping characteristics of the first damping element and the second damping element are configured to provide a greater amount of motion damping to the accelerometer than to the gyroscope.

in some embodiments, the damping characteristics of the first damping element and the second damping element comprise a stiffness of the first damping element and a stiffness of the second damping element, respectively, wherein the stiffness of the first damping element is less than the stiffness of the second damping element.

in some embodiments, the stiffness of the first damping element is configured to reduce noise associated with signals generated by the accelerometer and the stiffness of the second damping element is configured to reduce noise associated with signals generated by the gyroscope.

In some embodiments, the accelerometer comprises a microelectromechanical system (MEMS) accelerometer and the gyroscope comprises a MEMS gyroscope.

In some embodiments, the damping characteristics include a stiffness and/or viscoelasticity of the first and second damping elements.

In some embodiments, the damping characteristic comprises a stiffness of the first damping element and the second damping element, wherein the stiffness of the first damping element is less than the stiffness of the second damping element.

In some embodiments, the first and second damping elements each comprise at least one of: a sponge, foam, rubber, gel, piezoelectric material, or shape memory material.

In some embodiments, the first and second damping elements each have an active and/or passive damping characteristic.

In some embodiments, the first and second damping elements each comprise at least one of: springs, pistons, hydraulic devices, air bags, dampers, bumpers, isolators.

In some embodiments, the first and second damping elements comprise springs having a spring rate and shock absorbers having a damping rate.

In some embodiments, the first inertial sensor is embedded within the first damping element or encased within the first damping element; and

The second inertial sensor is embedded in the second damping element or wrapped in the second damping element.

There is also provided an unmanned aerial vehicle comprising:

A body;

The fuselage carrying an apparatus configured for determining a spatial position of the drone, the apparatus comprising:

A support base carried by the body;

A first inertial sensor connected to the support base by a first damping element for damping movement of the first inertial sensor; and

a second inertial sensor is connected to the support base by a second damping element for damping movement of the second inertial sensor, wherein the first inertial sensor and the second inertial sensor each comprise a different sensor type, the first damping element and the second damping element having different damping characteristics.

in some embodiments, the first inertial sensor and the second inertial sensor require different amounts of motion damping, and the damping characteristics of the first damping element and the second damping element are each used to provide different amounts of damping.

In some embodiments, the first inertial sensor comprises an accelerometer and the second inertial sensor comprises a gyroscope, wherein the damping characteristics of the first damping element and the second damping element are configured to provide a greater amount of motion damping to the accelerometer than to the gyroscope.

In some embodiments, the damping characteristics of the first damping element and the second damping element comprise a stiffness of the first damping element and a stiffness of the second damping element, respectively, wherein the stiffness of the first damping element is less than the stiffness of the second damping element.

in some embodiments, the stiffness of the first damping element is configured to reduce noise associated with signals generated by the accelerometer and the stiffness of the second damping element is configured to reduce noise associated with signals generated by the gyroscope.

In some embodiments, the accelerometer comprises a microelectromechanical system (MEMS) accelerometer and the gyroscope comprises a MEMS gyroscope.

In some embodiments, the damping characteristics include a stiffness and/or viscoelasticity of the first and second damping elements.

in some embodiments, the damping characteristic comprises a stiffness of the first damping element and the second damping element, wherein the stiffness of the first damping element is less than the stiffness of the second damping element.

In some embodiments, the first and second damping elements each comprise at least one of: a sponge, foam, rubber, gel, piezoelectric material, or shape memory material.

In some embodiments, the first and second damping elements each have an active and/or passive damping characteristic.

In some embodiments, the first and second damping elements each comprise at least one of: springs, pistons, hydraulic devices, air bags, dampers, bumpers, isolators.

In some embodiments, the first and second damping elements comprise springs having a spring rate and shock absorbers having a damping rate.

In some embodiments, the first inertial sensor is embedded within the first damping element or encased within the first damping element; and

the second inertial sensor is embedded in the second damping element or wrapped in the second damping element.

In some embodiments, the support base is coupled to the UAV via a rigid coupling.

it is to be understood that different aspects of the invention may be understood separately, together or in combination with each other. The aspects of the invention described herein may be applied to any particular application or any other type of movable object set forth below. Any description of the aircraft herein may be applied to and used with any movable object, such as any vehicle. In addition, the systems, devices, and methods disclosed herein in the context of aeronautical (e.g., flying) sports may also be applied in the context of other types of sports, such as land or water based movement, underwater sports, or space sports. Further, any description herein of a rotor or rotor assembly may be applied to and used in any propulsion system, device, or apparatus configured to generate propulsion through rotation (e.g., propellers, wheels, shafts).

Other objects and features of the present invention will become apparent by a review of the specification, claims and appended figures.

Introduction front case

Any publications, patents, and patent applications mentioned in this specification are herein incorporated by reference to the same extent as if each individual publication, patent, or patent application was specifically and individually indicated to be incorporated by reference.

Drawings

The novel features of the invention are set forth with particularity in the appended claims. A better understanding of the features and advantages of the present invention will be obtained by reference to the following detailed description that sets forth illustrative embodiments, in which the principles of the invention are utilized, and the accompanying drawings of which:

FIG. 1 illustrates a sensing device with damping according to an embodiment

FIG. 2 illustrates a sensing device with separately damped sensors according to an embodiment;

FIG. 3 illustrates a sensing device having damped and undamped sensors according to an embodiment;

FIG. 4 illustrates a sensing device with separately damped sensors according to an embodiment;

FIG. 5 illustrates an unmanned aerial vehicle according to an embodiment;

Fig. 6 illustrates a movable object including a carrier and a payload, in accordance with an embodiment; and

Fig. 7 is a schematic diagram in block diagram form of a system for controlling a movable object, in accordance with an embodiment.

Detailed Description

The present disclosure provides an improved sensing device for determining the spatial position of a movable object, such as an Unmanned Aerial Vehicle (UAV). In some cases, a sensing device described herein may include one or more inertial sensors. The term "inertial sensor" may be used herein to refer to a motion sensor (e.g., velocity sensor, acceleration sensor such as an accelerometer), orientation sensor (e.g., gyroscope), or Inertial Measurement Unit (IMU) having one or more integrated motion sensors and/or one or more integrated orientation sensors. The inertial sensors may be connected to a support base carried by the movable object through respective damping elements. The amount of motion damping provided by the damping element may be optimized based on the inertial sensor type. For example, the damping element of the accelerometer may provide a different amount of damping than the damping element of the gyroscope. In existing sensing devices, different types of inertial sensors may be integrated into a single unit (e.g., IMU) and thus receive the same amount of damping, as opposed to the approach described herein, which enables tailoring the amount of damping for different sensor types. This may be advantageous in the following cases: different amounts of damping are required for different sensor types to achieve optimal performance. For example, high damping may improve the signal-to-noise ratio of an accelerometer, but may also increase the response delay of a gyroscope. Thus, the sensing devices described herein may be used in conjunction with a control system of a movable object in order to improve the stability, response time, and accuracy and precision of control of the movable object.

Embodiments of the sensing devices described herein may be carried by a movable object (such as by a movable object provided below). The sensing means may be located on any suitable part of the movable object, such as above, below, on a side of the movable object or inside the body. In some cases, the sensing device is mechanically coupled to the movable object such that the spatial position and/or motion of the movable object corresponds to the spatial position and/or motion sensed by the sensing device. The sensing device may be connected to the moveable object by a rigid connection such that the sensing device does not move relative to the portion of the moveable object to which it is attached. Alternatively, the connection between the sensing device and the movable object may allow the sensing device to move relative to the movable object. The connection may be a permanent connection or a non-permanent (e.g., releasable) connection. Suitable attachment methods may include adhesives, bonding, welding, and/or fasteners (e.g., screws, nails, pins, etc.). Alternatively, the sensing means may be integrally formed with a portion of the moveable object. Further, the sensing device can be electrically coupled to a portion of the movable object (e.g., a processing unit, a control system, a data store) to facilitate enabling the sensed data collected by the sensing device to be used for various functions of the movable object (e.g., navigation, control, propulsion, communication with a user or other device, etc.).

The sensing means may comprise one or more sensors for determining the current state of the movable object. Exemplary sensors suitable for use in conjunction with embodiments described herein may include location sensors (e.g., Global Positioning System (GPS) sensors, mobile device transmitters implementing location triangulation), vision sensors (e.g., imaging devices such as cameras capable of detecting visible, infrared, or ultraviolet light), proximity sensors (e.g., ultrasonic sensors, lidar sensors), inertial sensors (e.g., accelerometers, gyroscopes, IMUs as described above), or field sensors (e.g., magnetometers, electromagnetic sensors). Any of the embodiments described herein for an inertial sensor may be applied to other types of sensors, and vice versa. The state information provided by the sensors may include information about the spatial position (e.g., position, orientation) of the movable object. The state information may also include information about the motion of the movable object (e.g., translational velocity, translational acceleration, angular velocity, angular acceleration, etc.). The sensor may be used, for example, to determine the spatial position and/or motion of the movable object with respect to at most six degrees of freedom (e.g., three positions and/or translational degrees of freedom, three orientations and/or rotational degrees of freedom). The state information may be provided for the overall reference frame, or for the reference frame of another entity. A processing unit may be utilized to receive and process status information generated by one or more sensors to facilitate determination of the spatial position and/or motion of the movable object. The spatial position and/or motion information may then be used for various applications, such as navigation, control, propulsion, communication, and so forth.

For example, the sensing device may include any suitable number and combination of inertial sensors, such as at least one, two, three, or more accelerometers, and/or at least one, two, three, or more gyroscopes. Optionally, the sensing device may include at least one, two, three, or more IMUs, each of which may include any number or combination of integrated accelerometers and gyroscopes. The inertial sensor may provide sensory data related to a single axis of motion. The axis of motion may correspond to an axis (e.g., a longitudinal axis) of the inertial sensor. In embodiments where the apparatus comprises a plurality of inertial sensors, each inertial sensor may provide measurements along a different axis of motion. For example, the sensing device may include three accelerometers to provide acceleration data along three different axes of motion. The three axes of motion may be orthogonal axes. One or more of the accelerometers may be a linear accelerometer that measures acceleration along a translational axis. Conversely, one or more of the accelerometers may be used for angular accelerometers that measure acceleration about an axis of rotation. As another example, the sensing device may include three gyroscopes to provide orientation data about three different axes of rotation. The three axes of rotation may be orthogonal axes (e.g., roll, pitch, yaw). Alternatively, at least some or all of the inertial sensors may provide measurements relating to the same axis of motion. Such redundancy may be implemented, for example, to improve measurement accuracy. Optionally, the inertial sensor may be capable of providing sensory data relating to a plurality of axes. For example, an IMU including multiple integrated accelerometers and gyroscopes may be used to generate acceleration data and orientation data for up to six axes of motion. Alternatively, a single accelerometer may be used to detect acceleration along multiple axes, and a single gyroscope may be used to detect rotation about multiple axes.

Various inertial sensor configurations and implementations may be incorporated into the sensing devices described herein. For example, the length or width of the inertial sensor may be less than or equal to approximately 20 microns, 50 microns, 100 microns, 200 microns, 500 microns, 1mm, 2mm, 3mm, 4mm, 5mm, 6mm, 7mm, 8mm, 9mm, 10mm, 15mm, 20mm, 30mm, 40mm, or 50 mm. Conversely, the length or width of the inertial sensor may be greater than or equal to about 20 microns, 50 microns, 100 microns, 200 microns, 500 microns, 1mm, 2mm, 3mm, 4mm, 5mm, 6mm, 7mm, 8mm, 9mm, 10mm, 15mm, 20mm, 30mm, 40mm, or 50 mm. Some or all of the inertial sensors described herein may be micro-electromechanical system (MEMS) sensors that may be smaller than other types of inertial sensors. Such MEMS sensors may be provided as part of an integrated circuit, such as within a chip.

The sensing device may comprise a component, such as a support base, adapted to support the sensor. The support base may include a housing, plate, wall, platform, frame, or any other suitable element for mounting and securing the sensor. The support base may be approximately flat or planar. Rather, the support base may be shaped as a cube, prism, cylinder, sphere, hemisphere, or any other suitable three-dimensional geometry. The support base may be hollow or solid. In addition, the support base may be formed as a single element or as a plurality of discrete elements. In the latter embodiment, the individual discrete elements of the support base may be located on different parts of the movable object. In some cases, the support base may be attached to or integrally formed with a housing or body of the movable object. The support base may be rigidly connected to the movable object such that movement of the support base corresponds to movement of the movable object. Alternatively, the support base may be allowed to move relative to the movable object. The material properties of the support base may be varied as desired. For example, the support base may be formed from a relatively rigid material. Alternatively, the support base may be formed from a relatively compliant material. Optionally, the support base may comprise an electrical coupling element (e.g. wire, circuit) adapted to electrically couple the sensor to another element as described herein before; alternatively, the support base may be used to house such electrical coupling elements.

The sensors described herein may be attached to the support base in any suitable arrangement. For example, one or more of the sensors may be attached to a top surface, a bottom surface, a side surface, an outer surface, and/or an inner surface of the support base. Different sensors may be attached to different parts of the support base. In some cases, a plurality of sensors may each be coupled to the support base in an arrangement that maintains a predetermined spatial relationship between the sensors. For example, a plurality of sensors may each be attached to a respective orthogonal wall of the support base such that the plurality of sensors are oriented orthogonally to each other. Alternatively, at least some of the plurality of sensors may be arranged parallel to each other. The sensor may be connected to the support base using any suitable connection mechanism, such as the connection mechanisms described previously herein. The sensor may be directly attached to the support base or indirectly attached to the support base through one or more intermediate elements. The sensor may contact the support base directly or indirectly when connected.

In some cases, the sensor may be indirectly coupled to the support base through a damping element. The damping element may be any element suitable for damping the motion of an attached sensor, such as an active damping element, a passive damping element, or a hybrid damping element having both active and passive damping characteristics. The motion damped by the damping elements provided herein may include one or more of a shock, oscillation, slosh, or impact. Such motion may result from motion of the movable object transmitted to the sensor through the support base. The damping element may provide motion damping by isolating the sensor from unwanted sources of motion in the following manner: dissipate or reduce the amount of motion (e.g., shock isolation) transmitted to the sensor. The damping element may reduce the magnitude (e.g., amplitude) of motion that would otherwise be experienced by the sensor, such as a magnitude reduction greater than or equal to about 10%, 20%, 30%, 40%, 50%, 60%, 70%, 80%, 90%, or 100%. In some cases, the damping element may be configured to reduce motion with a particular frequency. For example, some damping elements may reduce high frequency motion, while other damping elements may reduce low frequency motion. The damping element may damp movements having the following frequencies: greater than or equal to about 0.5Hz, 1Hz, 5Hz, 10Hz, 20Hz, 30Hz, 40Hz, 50Hz, 100Hz, 200Hz, 300Hz, 400Hz, 500Hz, 600Hz, 700Hz, 800Hz, 900Hz, or 1000 Hz. Alternatively, the damping element may damp movements having the following frequencies: less than or equal to about 0.5Hz, 1Hz, 5Hz, 10Hz, 20Hz, 30Hz, 40Hz, 50Hz, 100Hz, 200Hz, 300Hz, 400Hz, 500Hz, 600Hz, 700Hz, 800Hz, 900Hz, or 1000 Hz. The motion damping applied by the damping element may improve the quality of the sensor signal generated by the sensor, such as by reducing the amount of noise and/or measurement drift of the sensor, and by increasing the accuracy, precision, responsiveness, and/or stability of the sensor, which may also improve the quality of the sensor signal generated by the sensor by increasing the accuracy, precision, responsiveness, and/or stability of the sensor.

The damping elements described herein may be formed from any suitable material or combination of materials, including solid, liquid, or gaseous materials. The material for the damping element may be compressible and/or deformable. For example, the damping element may be a sponge, a foam, a rubber material, a gel, or the like. Alternatively or additionally, the damping element may comprise a piezoelectric material or a shape memory material. The damping element may include one or more mechanical elements such as springs, pistons, hydraulics, pneumatics, bumpers, shock absorbers, isolators or the like. The characteristics of the damping element may be selected so as to provide a predetermined amount of motion damping. For example, the damping element may have a characteristic stiffness that may correspond to the young's modulus of the damping element. The young's modulus may be greater than or equal to about 0.01GPa, ().05GPa, 0.1GPa, 0.2GPa, 0.3GPa, 0.4GPa, 0.5GPa, 0.6GPa, 0.7GPa, 0.8GPa, 0.9GPa, 1GPa, or 5 GPa. Alternatively, the Young's modulus may be less than or equal to about 0.01GPa, 0.05GPa, 0.1GPa, 0.2GPa, 0.3GPa, 0.4GPa, 0.5GPa, 0.6GPa, 0.7GPa, 0.8GPa, 0.9GPa, 1GPa, or 5 GPa. In some cases, the damping element may have viscoelastic properties. The damping element may be anisotropic or isotropic in its properties. For example, the damping element may provide motion damping equally in all directions of motion. Rather, the damping elements may provide motion damping in only a subset of directions of motion (e.g., in a single direction of motion).

The connections between the sensor and the damping element and between the damping element and the support base may use any suitable connection mechanism, such as those described hereinbefore. Moreover, although embodiments herein may be depicted as utilizing a single damping element coupled to a single sensor, it should be understood that any suitable combination of damping elements and sensors may be used. For example, a single sensor may be connected to the support base using multiple damping elements. Each damping element may be attached to a different portion (e.g., an upper surface, a lower surface, a side surface, an inner surface, and/or an outer surface) of the sensor. In some cases, the sensor may be embedded within the damping element or enclosed by the damping element. Alternatively, the damping element may be attached only to a particular portion of the sensor (e.g., only to a single surface of the sensor).

Turning now to the drawings, FIG. 1 illustrates a sensing device 100 with damping according to an embodiment. The sensing device 100 can include at least one inertial sensor 102 coupled to a support base 104 via a damping element 106. In some cases, the inertial sensor 102 may be an IMU having any suitable combination of accelerometers and gyroscopes, such as a combination of one or more accelerometers 108 and one or more gyroscopes 110. The accelerometer 108 and gyroscope 110 may be integrated into an IMU such that the inertial sensor 102 is provided as a single component (e.g., a single chip). The sensing device 100 may include a processing unit (not shown) connected to the inertial sensors 102 for receiving and processing sensor signals from the one or more accelerometers 108 and the one or more gyroscopes 110, and thereby determining acceleration and rotation of the sensing device 100.

The damping element 106, represented herein as a spring 112 and a damper 114, may provide motion damping to the inertial sensor 102. The spring 112 may be characterized by an elastic coefficient representing the elastic properties of the damping element 106, while the damper 114 may be characterized by a damping coefficient representing the viscous properties of the damping element 106. Although fig. 1 depicts a single spring 112 and damper 114 in parallel, the damping element 106, as with all other damping elements provided herein, may be represented by any number, combination, and arrangement of springs, dampers, or other representative components, each characterized by a respective coefficient corresponding to a characteristic (e.g., stiffness, viscoelasticity) of the damping element 106. In some cases, the damping element 106 may be represented by a single component (e.g., a single spring, a single damper) rather than multiple components. The amount of motion damping provided by the damping element 106 may be determined based on the characteristics of the damping element 106. In embodiments where the accelerometer 108 and the gyroscope 110 are integrated into the inertial sensor 102 so as to form a single component, the motion damping provided by the damping element 106 may be applied uniformly to the accelerometer 108 and the gyroscope 110 such that the accelerometer 108 and the gyroscope 110 receive the same or similar amount of motion damping.

Fig. 2 illustrates a sensing device 200 with separately damped sensors according to an embodiment. The sensing device 200 can include a plurality of sensors, such as a first inertial sensor 202 and a second inertial sensor 204. The plurality of sensors may be coupled to the support base 206 by a plurality of damping elements. For example, the first and second inertial sensors 202, 204 may be coupled to the support base 206 by respective first and second damping elements 208, 210. The sensors of the sensing device 200 can each be coupled to the support base 206 through different damping elements. Alternatively, at least some of the sensors may be connected to the support base 206 by the same damping element. In some cases, the plurality of sensors, including the first inertial sensor 202 and the second inertial sensor 204, may be connected to a processing unit (not shown) for receiving and processing signals generated by the sensors to determine spatial position and/or motion (e.g., acceleration and/or rotation) of the sensing device 200.

The first and second damping elements 208, 210 may have any suitable material characteristics. For example, the first damping element 208 may be represented by a first spring 212 characterized by a first spring rate and a first damper 214 characterized by a first damping rate. The second damping element 210 may be represented by a second spring 216 characterized by a second spring coefficient and a second damper 218 characterized by a second damping coefficient. The first spring rate and the first damping rate may represent characteristics of the first damping element 208, and the second spring rate and the second damping rate may represent characteristics of the second damping element 210.

In some cases, the first inertial sensor 202 is a different sensor type than the second inertial sensor 204. For example, the first inertial sensor 202 may include one or more accelerometers and the second inertial sensor 204 may include one or more gyroscopes, or vice versa. The properties (e.g. stiffness, visco-elasticity) of the first damping element 208 may be different from the properties of the second damping element 2] 0. For example, the first damping element 208 may be less rigid than the second damping element 210, or vice versa. Thus, the amount of motion damping applied to the first inertial sensor 202 may be different (e.g., greater than, less than) the amount applied to the second inertial sensor 204. For example, the motion damping applied to the first inertial sensor 202 may be approximately 10%, 20%, 30%, 40%, 50%, 60%, 70%, 80%, or 90% of the motion damping applied to the second inertial sensor 204, or vice versa. Conversely, the amount of motion damping applied to the first inertial sensor 202 may be approximately 110%, 120%, 130%, 140%, 150%, 160%, 170%, 180%, 190%, 200%, 300%, 400%, or 500% of the motion damping applied to the second inertial sensor 204, or vice versa.

In some cases, the amount of motion damping applied to first and second inertial sensors 202 and 204 by first and second damping elements 208 and 210, respectively, may be selected based on the amount of damping required to optimize or improve the performance of first and second inertial sensors 202 and 204 (e.g., performance related to reducing noise and/or accuracy while maintaining satisfactory accuracy, precision, responsiveness, and/or stability). For example, as discussed earlier above, a larger amount of motion damping may be beneficial for accelerometers, while a smaller amount of motion damping may be beneficial for gyroscopes. Since the inertial sensors 202, 204 are provided as separate components rather than being integrated into a single component, the amount of damping can be varied individually for each sensor. Thus, depending on the sensor type of the inertial sensor connected, the characteristics (e.g., stiffness) of the damping elements 208, 210 may be selected so as to provide an appropriate amount of motion damping. For example, the first inertial sensor 202 may be an accelerometer and the second inertial sensor 204 may be a gyroscope. The damping provided by the first damping element 208 to the first inertial sensor 202 may be greater than the damping provided by the second damping element 210 to the second inertial sensor 204.

Fig. 3 shows a sensing device 300 with damped and undamped sensors according to an embodiment. The sensing device 300 can include a plurality of sensors, such as a first inertial sensor 302 and a second inertial sensor 304. The first inertial sensor 302 may be connected to the support base 306 without any intervening elements to provide motion damping. In some cases, the first inertial sensor 302 can be directly connected to the support base 306. The second inertial sensor 304 may be connected to the support base 306 by a damping element 308, the damping element 308 being represented herein by a spring 310 characterized by a spring rate and a damper 312 characterized by a damping rate. The first inertial sensor 302 may be of a type that does not require motion damping to produce sensed data of optimal or most desirable quality. For example, the first inertial sensor 302 may include one or more gyroscopes. Conversely, the second inertial sensor 304 may be a type of sensor that exhibits improved performance when motion damping is applied. For example, the second inertial sensor 304 may include one or more accelerometers. Similar to other embodiments described previously herein, the characteristics of the damping element 308 may be selected to provide an appropriate amount of motion damping to the second inertial sensor 304. Similar to other embodiments provided herein, the first and second inertial sensors 302, 304 can be connected to a processing unit configured to process sensing signals received from the first and second inertial sensors 302, 304.

Fig. 4 illustrates a sensing device 400 with separately damped sensors according to an embodiment. The sensing device 400 can include a plurality of inertial sensors coupled to a support base 402, including at least a first inertial sensor 404 and a second inertial sensor 406. Although only two inertial sensors 404, 406 are depicted herein, it should be understood that sensing device 400, like any of the sensing devices described herein, may include any suitable number of inertial sensors. The first inertial sensor 404 may be an IMU that includes one or more integrated accelerometers 408 and one or more integrated gyroscopes 410. Similarly, the second inertial sensor 406 may be an IMU that includes one or more integrated accelerometers 412 and one or more integrated gyroscopes 414.

The plurality of inertial sensors of the sensing device 400 can be coupled to the support base 402 via a plurality of damping elements. For example, the first inertial sensor 404 and the second inertial sensor 406 may be coupled to the support base 402 via a first damping element 416 and a second damping element 418, respectively. The first damping element 416 and the second damping element 418 may each be represented by a suitable combination of spring and damper as previously discussed. In some cases, one or more of the plurality of inertial sensors can be connected to the support base 402 by more than one damping element (e.g., by two, three, four, five, or more damping elements). Conversely, one or more of the inertial sensors may be directly connected to the support base 402 without any damping elements. Optionally, some of the sensors of the sensing device 400 may be connected to the support base 402 by the same damping element.

Similar to the embodiment of the sensing device 200, the characteristics of the various damping elements may differ from one another. For example, the characteristics of the first damping element 416 may be different than the characteristics of the second damping element 418. In some cases, the first damping element 416 may be less rigid than the second damping element 418, or vice versa. Thus, the amount of motion damping applied to the first inertial sensor 404 may be different (e.g., greater than, less than) the amount applied to the second inertial sensor 406. For example, the motion damping applied to the first inertial sensor 404 may be approximately 0%, 10%, 20%, 30%, 40%, 50%, 60%, 70%, 80%, or 90% of the motion damping applied to the second inertial sensor 406, or vice versa. Conversely, the amount of motion damping applied to the first inertial sensor 404 may be approximately 110%, 120%, 130%, 140%, 150%, 160%, 170%, 180%, 190%, 200%, 300%, 400%, or 500% of the motion damping applied to the second inertial sensor 406, or vice versa.

In some cases, the amount of motion damping applied to the first and second inertial sensors 404, 406 by the first and second damping elements 416, 418, respectively, may be selected based on the amount of damping required to optimize or improve the performance of one of the first and second inertial sensors 404, 406. For example, the amount of damping applied by the first damping element 416 may be selected based on the damping requirements of the accelerometer 408 of the first inertial sensor 404, while the amount of damping applied by the second damping element 418 may be selected based on the damping requirements of the gyroscope 414 of the second inertial sensor 406. In such embodiments, the first damping element 416 may be less stiff than the second damping element 418 so as to provide an amount of motion damping that is greater than the second damping element 418.

As mentioned previously, some of the sensors of the sensing device 400 may be connected to the support base 402 by the same damping elements. Thus, one or more damping elements of the sensing device 400 can be coupled to more than one inertial sensor. The shared damping element may provide the same or similar amount of motion damping to the connected sensors. This approach may be beneficial for sensors with similar damping requirements.

The sensing device 400 may be connected to a processing unit (not shown) for receiving sensing signals from each of a plurality of sensors including a first inertial sensor 404 and a second inertial sensor 406. Optionally, some of the sensing signals received by the processing unit may be redundant to other sensing signals. For example, the processing unit may receive more than one signal indicative of acceleration, more than one signal indicative of rotation, and so forth. The processing unit may process the received signals in any suitable manner in order to determine the spatial position and/or motion. For example, the processing unit may average some or all of the received sensor signals. Alternatively, the processing unit may process some or all of the received signals using a redundant method. The redundancy method, when used for a received signal that is a continuous value, may include: an intermediate value between one or more of the received signal values (e.g., an average of the received signal values) is determined and output as a processing result. The redundancy method, when used for a received signal that is a discrete value, may comprise: a value is determined that is closest to or equal to a majority of the received signal values and the value is output as a result of the processing.

in some cases, the processing unit may receive signals only from the type of sensors in the first and second inertial sensors 404 and 406 for which motion damping is optimized or improved (referred to herein as "optimized sensors"). For example, the processing unit may receive acceleration signals only from the accelerometer 408 of the first inertial sensor 404 and rotation signals only from the gyroscope 414 of the second inertial sensor 406. Alternatively, the processing unit may receive sensor signals from all sensor types in both the first and second inertial sensors 404, 406, but may only utilize signals from optimized sensors when determining the spatial position of the movable object. Conversely, the processing unit may utilize all signals from all sensor types to determine the spatial location, but may assign greater weight to the signals from the optimized sensors (e.g., a weighted average). Advantageously, such an approach may realize the benefit of tailoring the damping applied to an inertial sensor (e.g., IMU) comprising an integrated accelerometer and an integrated gyroscope.

The systems, devices, and methods described herein may be applied to a wide range of movable objects. As mentioned previously, any description of the aircraft herein may be applied to and used with any movable object. The movable object of the present invention may be used to move within any suitable environment, such as in the air (e.g., a fixed wing aircraft, a rotorcraft, or an aircraft with neither fixed wings nor rotors), in water (e.g., a boat or submarine), on the ground (e.g., a motor vehicle such as a car, truck, bus, truck, motorcycle; a movable structure or frame such as a cane, fishing pole, or train), underground (e.g., a subway), in space (e.g., a space shuttle, satellite, or probe), or any combination of these environments. The movable object may be a vehicle, such as the vehicles described elsewhere herein. In some embodiments, the movable object may be mounted on a living body, such as a human or animal. Suitable animals may include birds, canines, felines, equines, bovines, ovines, porcines, dolphins, rodents, or insects.

The movable object may be able to move freely within the environment with respect to six degrees of freedom (e.g., three translational degrees of freedom and three rotational degrees of freedom). Alternatively, the movement of the movable object may be limited for one or more degrees of freedom, such as by a predetermined path, trajectory, or orientation. The movement may be actuated by any suitable actuation mechanism, such as an engine or motor. The actuating mechanism of the movable object may be powered by any suitable energy source, such as electrical energy, magnetic energy, solar energy, wind energy, gravitational potential energy, chemical energy, nuclear energy, or any suitable combination thereof. The movable object may be self-propelled by a propulsion system as described elsewhere herein. The propulsion system may optionally be operated by means of an energy source such as electric energy, magnetic energy, solar energy, wind energy, gravitational potential energy, chemical energy, nuclear energy, or any suitable combination thereof. Alternatively, the movable object may be carried by a living organism.

In some cases, the movable object may be a vehicle. Suitable vehicles may include marine vehicles, air vehicles, space vehicles, or land vehicles. For example, the aerial vehicle may be a fixed wing aircraft (e.g., airplane, glider), a rotorcraft (e.g., helicopter, rotorcraft), an aircraft having both fixed wings and rotors, or an aircraft having neither fixed wings nor rotors (e.g., airship or hot air balloon). The vehicle may be self-propelled, such as in the air, above or below water, in space, or self-propelled, either onshore or underground. Self-propelled vehicles may utilize a propulsion system, such as a propulsion system including one or more engines, motors, wheels, shafts, magnets, rotors, propellers, blades, nozzles, or any suitable combination thereof. In some cases, the propulsion system may be used to enable the movable object to take off from a surface, land on a surface, maintain its current position and/or orientation (e.g., hover), change orientation, and/or change position.

The movable object may be remotely controlled by a user or locally controlled by an occupant located in or on the movable object. In some embodiments, the movable object is an unmanned mobile object, such as a UAV. An unmanned movable object such as a UAV may not allow an occupant to carry the movable object. The movable object may be controlled by a person or an autonomous control system (e.g., a computer control system), or any suitable combination thereof. The movable object may be an autonomous or semi-autonomous robot, such as a robot configured with artificial intelligence.

The movable object may have any suitable size and/or dimensions. In some embodiments, the movable object may have a size and/or dimensions that enable a human occupant to ride within or upon the vehicle. Alternatively, the movable object may have a smaller size and/or dimension than would enable a human occupant to ride within or upon the vehicle. The movable object may have a size and/or dimensions suitable for being lifted or carried by a person. Alternatively, the size and/or dimensions of the movable object may be larger than those suitable for being lifted or carried by a person. In some cases, the movable object may have a maximum dimension (e.g., length, width, height, diameter, diagonal length) that is less than or equal to about: 2cm, 5cm, 10cm, 50cm, 1m, 2m, 5m, or 10 m. The maximum dimension may be greater than or equal to about: 2cm, 5cm, 10cm, 50cm, 1m, 2m, 5m, or 10 m. For example, the distance between the spindles of opposing rotors of the movable object may be less than or equal to about: 2cm, 5cm, 10cm, 50cm, 1m, 2m, 5m, or 10 m. Alternatively, the distance between the shafts of the opposing rotors may be greater than or equal to about: 2cm, 5cm, 10cm, 50cm, 1m, 2m, 5m, or 10 m.

In some embodiments, the movable object may have a volume of less than 100cm x 100cm, less than 50cm x 30cm, or less than 5cm x 3 cm. The total volume of the movable object may be less than or equal to about: 1cm3, 2cm3, 5cm3, 10cm3, 20cm3, 30cm3, 40cm3, 50cm3, 60cm3, 70cm3, 80cm3, 90cm3, 100cm3, 150cm3, 200cm3, 300cm3, 500cm3, 750cm3, 1000cm3, 5000cm3, 10, 000cm3, 100, 000cm3, 1m3, or 10m 3. Conversely, the total volume of the movable object may be greater than or equal to about: 1cm3, 2cm3, 5cm3, 10cm3, 20cm3, 30cm3, 40cm3, 50cm3, 60cm3, 70cm3, 80cm3, 90cm3, 100cm3, 150cm3, 200cm3, 300cm3, 500cm3, 750cm3, 1000cm3, 5000cm3, 10, 000cm3, 100, 000cm3, 1m3, or 10m 3.

In some embodiments, the movable object may have a footprint (which may refer to the area of a lateral cross-section enclosed by the movable object) that is less than or equal to about: 32, 000cm2, 20, 000cm2, 10, 000cm2, 1, 000cm2, 500cm2, 100cm2, 50cm2, 10cm2, or 5cm 2. Conversely, the footprint may be greater than or equal to about: 32, 000cm2, 20, 000cm2, 10, 000cm2, 1, 000cm2, 500cm2, 100cm2, 50cm2, 10cm2, or 5cm 2.

In some cases, the weight of the movable object may not exceed 1000 kg. The movable object may have a weight of less than or equal to about: 1000kg, 750kg, 500kg, 200kg, 150kg, 100kg, 80kg, 70kg, 60kg, 50kg, 45kg, 40kg, 35kg, 30kg, 25kg, 20kg, 15kg, 12kg, 10kg, 9kg, 8kg, 7kg, 6kg, 5kg, 4kg, 3kg, 2kg, 1kg, 0.5kg, 0.1kg, 0.05kg, or 0.01 kg. Conversely, the weight may be greater than or equal to about: 1000kg, 750kg, 500kg, 200kg, 150kg, 100kg, 80kg, 70kg, 60kg, 50kg, 45kg, 40kg, 35kg, 30kg, 25kg, 20kg, 15kg, 12kg, 10kg, 9kg, 8kg, 7kg, 6kg, 5kg, 4kg, 3kg, 2kg, 1kg, 0.5kg, 0.1kg, 0.05kg, or 0.01 kg.

In some embodiments, the movable object may be small relative to the load carried by the movable object. As will be described in further detail below, the payload may include a payload and/or a carrier. In some examples, the ratio of the weight of the movable object to the weight of the load may be greater than, less than, or equal to about 1: 1. In some cases, the ratio of the weight of the movable object to the weight of the load may be greater than, less than, or equal to about 1: 1. Optionally, the ratio of the weight of the carrier to the weight of the load may be greater than, less than, or equal to about 1: 1. When desired, the ratio of the weight of the movable object to the weight of the load may be less than or equal to: 1: 2, 1: 3, 1: 4, 1: 5, 1: 10, or even less. Conversely, the ratio of the weight of the movable object to the weight of the load may also be greater than or equal to: 2: 1, 3: 1, 4: 1, 5: 1, 10: 1, or even greater.

In some embodiments, the movable object may have a low energy consumption. For example, the movable object may use less than about: 5W/h, 4W/h, 3W/h, 2W/h, 1W/h, or less. In some cases, the carrier of the movable object may have a low energy consumption. For example, the carrier may use less than about: 5W/h, 4W/h, 3W/h, 2W/h, 1W/h, or less. Optionally, the payload of the movable object may have a low energy consumption, such as less than about: 5W/h, 4W/h, 3W/h, 2W/h, 1W/h, or less.

Fig. 5 shows an Unmanned Aerial Vehicle (UAV)500 in accordance with an embodiment of the invention. The UAV may be an example of a movable object as described herein. The UAV500 may include a propulsion system having four rotors 502, 504, 506, and 508. Any number of rotors (e.g., one, two, three, four, five, six, or more) may be provided. The rotor may be an embodiment of a self-tightening rotor as described elsewhere herein. The rotors, rotor assemblies, or other propulsion systems of the unmanned aerial vehicle may enable the unmanned aerial vehicle to hover/maintain a position, change an orientation, and/or change a position. The distance between the spindles of the opposing rotors may be any suitable length 510. For example, the length 510 may be less than or equal to 2m, or less than or equal to 5 m. In some embodiments, the length 510 may be in a range of 40cm to 1m, 10cm to 2m, or 5cm to 5 m. Any description of the UAV herein may apply to movable objects, such as different types of movable objects, or vice versa.

In some embodiments, the movable object may be used to carry a load. The load may include one or more of passengers, cargo, devices, equipment, and the like. The load may be provided within the housing. The housing may be separate from or part of the housing of the movable object. Alternatively, the load may be provided with a housing when the movable object does not have a housing. Alternatively, no outer shell may be provided for portions of the load or for the entire load. The load may be rigidly fixed relative to the movable object. Optionally, the load may be movable relative to the movable object (e.g., translatable or rotatable relative to the movable object).

in some embodiments, the payload comprises a payload. The payload may be used to not perform any operation or function. Alternatively, the payload may be a payload (also referred to as a functional payload) that performs some operation or function. For example, the payload may include one or more sensors for monitoring one or more targets. Any suitable sensor may be incorporated into the payload, such as an image capture device (e.g., a camera), an audio capture device (e.g., a parabolic microphone), an infrared imaging device, or an ultraviolet imaging device. The sensors may provide static sensory data (e.g., photographs) or dynamic sensory data (e.g., video). In some embodiments, the sensor provides sensory data to a target of the payload. Alternatively or in combination, the payload may include one or more transmitters for providing signals to one or more targets. Any suitable emitter may be used, such as an illumination source or a sound source. In some embodiments, the payload includes one or more transceivers, such as for communicating with modules remote from the movable object. Optionally, the payload may be configured to interact with an environment or a target. For example, the payload may include a tool, an instrument, or a mechanism capable of manipulating an object, such as a robotic arm.

Optionally, the load may comprise a carrier. The carrier may be provided for the payload, and the payload may be connected to the movable object by the carrier, either directly (e.g., directly contacting the movable object) or indirectly (e.g., not contacting the movable object). Conversely, the payload may be mounted on the movable object without requiring a carrier. The payload may be integrally formed with the carrier. Alternatively, the payload may be releasably connected to the carrier. In some embodiments, the payload may comprise one or more payload elements, and one or more of the payload elements may be movable relative to the movable object and/or carrier, as described above.

the carrier may be integrally formed with the movable object. Alternatively, the carrier may be releasably connected to the movable object. The carrier may be directly or indirectly connected to the movable object. The carrier may provide support for the payload (e.g., carry at least a portion of the weight of the payload). The carrier may include suitable mounting structures (e.g., a pan-tilt platform) capable of stabilizing and/or guiding the movement of the payload. In some embodiments, the carrier may be adapted to control a state (e.g., position and/or orientation) of the payload relative to the movable object. For example, the carrier may be used to move relative to the movable object (e.g., relative to one, two, or three translational degrees of freedom and/or one, two, or three rotational degrees of freedom) such that the payload maintains its position and/or orientation relative to a suitable frame of reference regardless of how the movable object moves. The reference frame may be a fixed reference frame (e.g., ambient environment). Alternatively, the reference frame may be a moving reference frame (e.g., the movable object, payload target).

in some embodiments, the carrier may be configured to allow the payload to move relative to the carrier and/or movable object. The movement may be a translation with respect to at most three degrees of freedom (e.g., along one, two, or three axes) or a rotation with respect to at most three degrees of freedom (e.g., about one, two, or three axes), or any suitable combination thereof.

In some cases, the carrier may include a carrier frame assembly and a carrier actuation assembly. The carrier frame assembly may provide structural support for the payload. The carrier frame assembly may comprise individual carrier frame components, some of which may be movable relative to each other. The carrier actuation assembly may include one or more actuators (e.g., motors) that actuate movement of the individual carrier frame components. The actuator may allow for simultaneous movement of multiple carrier frame parts or may be used to allow movement of only a single carrier frame part at a time. Movement of the carrier frame member may result in corresponding movement of the payload. For example, the carrier actuation assembly may cause one or more carrier frame members to rotate about one or more rotational axes (e.g., roll, pitch, or yaw axes). Rotation of the one or more carrier frame members may rotate the payload relative to the movable object about one or more axes of rotation. Alternatively or in combination, the carrier actuation assembly may cause one or more carrier frame components to translate along one or more translation axes, and thereby translate the payload relative to the movable object along one or more corresponding axes.

in some embodiments, movement of the movable object, carrier, and payload relative to a fixed reference frame (e.g., ambient environment) and/or each other may be controlled by a terminal. The terminal may be a remote control located remotely from the movable object, carrier, and/or payload. The terminal may be disposed on or secured to a support platform. Alternatively, the terminal may be a handheld or wearable device. For example, the terminal may include a smartphone, a tablet, a laptop, a computer, glasses, gloves, a helmet, a microphone, or a suitable combination thereof. The terminal may include a user interface such as a keyboard, mouse, joystick, touch screen, or display. Any suitable user input may be used to interact with the terminal, such as manually entering commands, voice control, gesture control, or position control (e.g., interacting through movement, position, or tilt of the terminal).

The terminal may be used to control any suitable state of the movable object, carrier, and/or payload. For example, the terminal may be used to control the position and/or orientation of the movable object, carrier, and/or payload relative to a fixed reference frame and/or each other. In some embodiments, the terminal may be used to control individual elements of the movable object, carrier, and/or payload, such as an actuation assembly of the carrier, a sensor of the payload, or a transmitter of the payload. The terminal may comprise wireless communication means adapted to communicate with one or more of the movable object, carrier, or payload.

The terminal may comprise a suitable display unit for viewing information of the movable object, carrier, and/or payload. For example, the terminal may be used to display information about the movable object, carrier, and/or payload in relation to position, translational velocity, translational acceleration, orientation, angular velocity, angular acceleration, or any suitable combination thereof. In some embodiments, the terminal can display information provided by the payload, such as data provided by a functional payload (e.g., images recorded by a camera or other image capture device).

Optionally, the same terminal may both control the movable object, carrier, and/or payload, or the state of the movable object, carrier, and/or payload, and receive and/or display information from the movable object, carrier, and/or payload. For example, a terminal may control the positioning of the payload relative to the environment while displaying image data captured by the payload, or information relating to the location of the payload. Alternatively, different terminals may be used for different functions. For example, a first terminal may control movement or state of the movable object, carrier, and/or payload, while a second terminal may receive and/or display information from the movable object, carrier, and/or payload. For example, a first terminal may be used to control the positioning of the payload relative to the environment while a second terminal displays image data captured by the payload. Various modes of communication may be utilized between the movable object and an integrated terminal that both controls the movable object and receives data, or between the movable object and multiple terminals that both control the movable object and receive data. For example, at least two different communication modes may be formed between the movable object and a terminal that both controls the movable object and receives data from the movable object.

Fig. 6 shows a movable object 600 comprising a carrier 602 and a payload 604 according to an embodiment. Although the movable object 600 is depicted as an aircraft, this description is not intended to be limiting, and any suitable type of movable object may be used as previously described herein. Those skilled in the art will appreciate that any of the embodiments described herein in the context of an aircraft system may be applied to any suitable movable object (e.g., a UAV). In some cases, the payload 604 may be provided on the movable object 600 without requiring a carrier 602. The moveable object 600 may include a propulsion mechanism 606, a sensing system 608, and a communication system 610.

As previously described, the propulsion mechanism 606 may include one or more of a rotor, propeller, blade, engine, motor, wheel, shaft, magnet, or nozzle. The movable object may have one or more, two or more, three or more, or four or more propulsion mechanisms. These propulsion mechanisms may all be of the same type. Alternatively, one or more of the propulsion mechanisms may be a different type of propulsion mechanism. The propulsion mechanism 606 may be mounted on the moveable object 600 using any suitable means. The propulsion mechanism 606 may be mounted on any suitable portion of the moveable object 600, such as the top, bottom, front, back, sides, or a suitable combination thereof.

In some embodiments, propulsion mechanism 606 may enable movable object 600 to vertically takeoff from a surface or vertically land on a surface without requiring any horizontal movement of movable object 600 (e.g., without taxiing along a runway). Optionally, the propulsion mechanism 606 may be operated to allow the movable object 600 to hover at a particular location and/or orientation in the air. One or more of the propulsion mechanisms 600 may be controlled independently of the other propulsion mechanisms. Alternatively, the propulsion mechanisms 600 may be used for simultaneous control. For example, the movable object 600 may have a plurality of horizontally oriented rotors that may provide lift and/or thrust to the movable object. The plurality of horizontally oriented rotors can be actuated to provide vertical takeoff, vertical landing, and hovering capabilities for the movable object 600. In some embodiments, one or more of the horizontally oriented rotors may rotate in a clockwise direction while one or more of the horizontally oriented rotors may rotate in a counterclockwise direction. For example, the number of clockwise rotors may be equal to the number of counterclockwise rotors. The rate of rotation of each of the horizontally oriented rotors can be individually varied to facilitate control of the lift and/or thrust generated by each rotor and thereby adjust the spatial position, velocity, and/or acceleration (e.g., with respect to at most three translational degrees of freedom and at most three rotational degrees of freedom) of the movable object 600.

The sensing system 608 may include one or more sensors that may sense spatial position, velocity, and/or acceleration (e.g., with respect to at most three translational degrees of freedom and at most three rotational degrees of freedom) of the movable object 600. The one or more sensors may include a GPS sensor, a motion sensor, an inertial sensor, a proximity sensor, or an image sensor. In some cases, the sensing system 608 can include embodiments of the sensing devices described previously herein. The sensing data provided by the sensing system 608 may be used to determine and/or control the spatial position, velocity, and/or orientation of the movable object 600 (e.g., using a suitable processing unit and/or control module as described below). Alternatively, the sensing system 608 may be used to provide data about the environment surrounding the movable object, such as weather conditions, proximity to potential obstacles, location of geographic features, location of man-made buildings, and the like.

The communication system 610 enables communication with a terminal 612 having a communication system 614 via wireless signals 616. The communication systems 610, 614 may include any number of transmitters, receivers, and/or transceivers suitable for wireless communication. The communication may be a one-way communication such that data is transmitted in only one direction. For example, one-way communication may involve only the movable object 600 transmitting data to the terminal 612, or vice versa. The data may be transmitted from one or more transmitters of the communication system 610 to one or more receivers of the communication system 612, or vice versa. Alternatively, the communication may be a two-way communication, such that data may be transmitted in both directions between the movable object 600 and the terminal 612. The two-way communication may involve transmitting data from one or more transmitters of the communication system 610 to one or more receivers of the communication system 614, and vice versa.

In some embodiments, the terminal 612 may provide control data to one or more of the movable object 600, carrier 602, and payload 604 and receive information from one or more of the movable object 600, carrier 602, and payload 604 (e.g., position and/or motion information of the movable object, carrier, or payload; data sensed by the payload, such as image data captured by a payload camera). In some cases, the control data from the terminal may include instructions for the relative position, movement, actuation, or control of the movable object, carrier, and/or payload. For example, the control data may result in a modification of the position and/or orientation of the movable object (e.g., by controlling propulsion mechanism 606), or a movement of the payload relative to the movable object (e.g., by controlling the carrier 602). The control data from the terminal may result in control of the payload, such as control of the operation of a camera or other image capture device (e.g., taking a still or moving picture, zooming, turning on or off, switching imaging modes, changing image resolution, changing focus, changing depth of field, changing exposure time, changing angle of view or field of view). In some cases, the communication from the movable object, carrier, and/or payload may include information from one or more sensors (e.g., of sensing system 608 or payload 604). The communication may include sensory information from one or more different types of sensors (e.g., GPS sensors, motion sensors, inertial sensors, proximity sensors, or image sensors). Such information may relate to the position (e.g., orientation), movement, or acceleration of the movable object, carrier, and/or payload. Such information from the payload may include data acquired by the payload or a sensed state of the payload. The control data provided or transmitted by the terminal 612 may be used to control the state of one or more of the movable object 600, the carrier 602, or the payload 604. Alternatively or in combination, the carrier 602 and the payload 604 may each further comprise a communication module for communicating with the terminal 612, such that the terminal may communicate with and control each of the movable object 600, carrier 602 and payload 604 individually.

In some embodiments, the movable object 600 may be used to communicate with another remote device in addition to the terminal 612 or instead of the terminal 612. Like the movable object 600, the terminal 612 may also be used to communicate with another remote device. For example, the movable object 600 and/or the terminal 612 may communicate with another movable object, or a carrier or payload of another movable object. The remote device may be a second terminal or other computing device (e.g., a computer, laptop, tablet, smartphone, or other mobile device) if desired. The remote device may be used to transmit data to the movable object 600, receive data from the movable object 600, transmit data to the terminal 612, and/or receive data from the terminal 612. Optionally, the remote device may be connected to the internet or other telecommunications network so that data received from the movable object 600 and/or the terminal 612 may be uploaded to a website or server.

Fig. 7 is a schematic diagram in block form of a system 700 for controlling a movable object, according to an embodiment. The system 700 may be used in conjunction with any suitable implementation of the systems, devices, and methods disclosed herein. The system 700 may include a sensing module 702, a processing unit 704, a non-transitory computer-readable medium 706, a control module 708, and a communication module 710.

The sensing module 702 may utilize different types of sensors that collect information related to the movable object in different ways. Different types of sensors may sense different types of signals or signals from different sources. For example, the sensors may include inertial sensors, GPS sensors, proximity sensors (e.g., lidar sensors), or vision/image sensors (e.g., cameras). The sensing module 702 may include any suitable implementation of the sensing devices previously described herein. The sensing module 702 may be operatively connected to a processing unit 704 having a plurality of processors. In some embodiments, the sensing module may be operatively connected to a transmission module 712 (e.g., a Wi-Fi image transmission module), the transmission module 712 being configured to transmit the sensed data device directly to a suitable external device or system. For example, the transmission module 712 may be used to transmit images captured by the camera of the sensing module 702 to a remote terminal.

The processing unit 704 may have one or more processors, such as a programmable processor (e.g., a Central Processing Unit (CPU)). The processing unit 704 may be operatively connected to a non-transitory computer-readable medium 706. The non-transitory computer-readable medium 706 may store logic, code, and/or program instructions that are executable by the processing unit 704 to perform one or more steps. The non-transitory computer-readable medium may include one or more memory units (e.g., a removable medium or an external memory such as an SD card or a Random Access Memory (RAM)). In some implementations, data from the sensing module 702 can be directly transferred to and stored in a memory unit of the non-transitory computer-readable medium 706. The memory unit of the non-transitory computer-readable medium 706 may store logic, code, and/or program instructions that are executable by the processing unit 704 to perform any suitable implementation of the methods described herein. For example, the processing unit 704 may be configured to execute the following instructions: cause the one or more processors of the processing unit 704 to analyze the sensory data generated by the sensing module. The memory unit may store sensed data from the sensing module to be processed by the processing unit 704. In some implementations, the memory unit of the non-transitory computer-readable medium 706 can be used to store processing results produced by the processing unit 704.

In some embodiments, the processing unit 704 may be operatively connected to a control module 708 for controlling the state of the movable object. For example, the control module 708 may be used to control a propulsion mechanism of the movable object to adjust the spatial position, velocity, and/or acceleration of the movable object with respect to six degrees of freedom. Alternatively or in combination, the control module 708 may control one or more states of a carrier, payload, or sensing module.

the processing unit 704 may be operatively connected to a communication module 710, the communication module 710 for transmitting and/or receiving data from one or more external devices (e.g., a terminal, a display device, or other remote controller). Any suitable communication means may be used, such as wired or wireless communication. For example, the communication module 710 may utilize one or more of a Local Area Network (LAN), a Wide Area Network (WAN), infrared, radio, WiFi, peer-to-peer (P2P) network, telecommunications network, cloud communication, and the like. Optionally, a relay station, such as a signal tower, satellite, or mobile station, may be used. The wireless communication may be short-range related or short-range unrelated. In some embodiments, the communication may or may not need to be in-line. The communication module 710 may transmit and/or receive one or more of sensing data from the sensing module 702, processing results generated by the processing unit 704, predetermined control data, user commands from a terminal or a remote controller, and the like.

The components of the system 700 may be arranged in any suitable configuration. For example, one or more of the components of the system 700 may be located on the movable object, carrier, payload, terminal, sensing system, or another external device in communication with one or more of the above. Additionally, while fig. 7 depicts a single processing unit 704 and a single non-transitory computer-readable medium 706, those skilled in the art will appreciate that this is not intended to be limiting and that the system 700 may include multiple processing units and/or non-transitory computer-readable media. In some implementations, one or more of the multiple processing units and/or non-transitory computer-readable media may be located in different locations, such as on the movable object, a carrier, a payload, a terminal, a sensing module, another external device in communication with one or more of the above, or a suitable combination thereof, such that any suitable aspect of the processing and/or memory functions performed by the system 700 may occur at one or more of the aforementioned locations.

While preferred embodiments of the present invention have been shown and described herein, it will be obvious to those skilled in the art that such embodiments are provided by way of example only. Numerous variations, changes, and substitutions will now occur to those skilled in the art without departing from the invention. It should be understood that various alternatives to the embodiments of the invention described herein may be employed in practicing the invention. It is intended that the following claims define the scope of the invention and that methods and structures within the scope of these claims and their equivalents be covered thereby.