阅读说明：本技术 一种机载无人机反制系统 (Airborne unmanned aerial vehicle counter-braking system ) 是由 张玉祺 于 2020-12-10 设计创作，主要内容包括：本发明公开了一种机载无人机反制系统,包括无人机反制设备、无人机和无人机地面站；所述无人机反制设备包括定位模块、控制模块、反制模块和电源模块；所述无人机内部设置有探测设备和处理器；所述探测设备设置有信号接收器和信号处理电路,所述处理器用于接收反制数据,并向所述反制模块发送反制指定无人机的指令；所述反制模块设置有无人机反制电路,所述反制模块接收到反制指定无人机的指令后,通过所述无人机反制电路对所述指定无人机进行无人机反制操作；本发明将探测设备和反制设备设置在无人机上,通过无人机在空中对进入巡检区域的无人机进行反制,避免了地面遮挡物的干扰,也不会对该区域的通信设备造成影响,提高了无人机反制效果。(The invention discloses an airborne unmanned aerial vehicle control system, which comprises unmanned aerial vehicle control equipment, an unmanned aerial vehicle and an unmanned aerial vehicle ground station; the unmanned aerial vehicle control device comprises a positioning module, a control module and a power module; the unmanned aerial vehicle is internally provided with a detection device and a processor; the detection device is provided with a signal receiver and a signal processing circuit, and the processor is used for receiving the countering data and sending an instruction for countering the designated unmanned aerial vehicle to the countering module; the control module is provided with an unmanned aerial vehicle control circuit, and after receiving an instruction for controlling a designated unmanned aerial vehicle, the control module performs unmanned aerial vehicle control operation on the designated unmanned aerial vehicle through the unmanned aerial vehicle control circuit; according to the unmanned aerial vehicle anti-jamming system, the detection equipment and the anti-jamming equipment are arranged on the unmanned aerial vehicle, and the unmanned aerial vehicle entering the inspection area is countered in the air by the unmanned aerial vehicle, so that the interference of ground shelters is avoided, the communication equipment in the area cannot be influenced, and the anti-jamming effect of the unmanned aerial vehicle is improved.)

1. The utility model provides an airborne unmanned aerial vehicle counter-system which characterized in that: the unmanned aerial vehicle control system comprises unmanned aerial vehicle control equipment, an unmanned aerial vehicle and an unmanned aerial vehicle ground station; the unmanned aerial vehicle counter-braking equipment is arranged inside the unmanned aerial vehicle; the unmanned aerial vehicle control device comprises a positioning module, a control module and a power module; the unmanned aerial vehicle is internally provided with a detection device and a processor; the unmanned aerial vehicle control device and the detection device are respectively in communication connection with the processor; the detection equipment is provided with a signal receiver and a signal processing circuit, and receives signals of the unmanned aerial vehicle ground station through the signal receiver; processing the signal of the ground station of the unmanned aerial vehicle through the signal processing circuit; the processor is used for receiving the reverse control data and sending an instruction for reversing the designated unmanned aerial vehicle to the reverse control module; the control module is provided with an unmanned aerial vehicle control circuit, and after receiving an instruction for controlling a designated unmanned aerial vehicle, the control module performs unmanned aerial vehicle control operation on the designated unmanned aerial vehicle through the unmanned aerial vehicle control circuit; the processor is connected with an unmanned aerial vehicle link of the unmanned aerial vehicle, and the unmanned aerial vehicle link transmits detection information sent by the detection equipment and the control data of the control equipment to the unmanned aerial vehicle ground station.

2. The airborne drone counteraction system of claim 1, wherein: the anti-modulation module comprises a signal generation unit, a power amplification unit and a signal transmitting unit; the signal transmitting unit is connected with the power amplifying unit; the signal generation unit is respectively connected with the control module, the power supply module and the power amplification unit.

3. The airborne drone counteraction system of claim 1, wherein: the power supply module is electrically connected with a power supply device of the unmanned aerial vehicle; the power module is respectively and electrically connected with the positioning module, the control module and the counter module.

4. The airborne drone counteraction system of claim 1, wherein: the unmanned aerial vehicle is provided with anti-interference equipment; the anti-interference navigation equipment comprises an information acquisition module, a calculation module and an anti-interference control module; the information acquisition module is used for acquiring the position information of a plurality of legal aircrafts in the current target control area in real time; the calculation module is used for determining the interference intensity of an interference signal sent by the unmanned aerial vehicle control device on each aircraft according to the position information of the plurality of aircraft and the working parameters of the unmanned aerial vehicle control device; and if the interference intensity of at least one target aircraft in the plurality of aircraft exceeds a preset interference intensity threshold value, the anti-interference control module controls the counter module to execute preset operation.

5. The airborne drone counteraction system of claim 4, wherein: the preset operation is a predefined operation for reducing the interference strength; the preset operation comprises controlling the unmanned aerial vehicle reverse braking equipment to stop sending out interference signals.

6. The airborne drone counteraction system of claim 4, wherein: the calculation module comprises a parameter acquisition unit, a first calculation unit and a second calculation unit; the parameter acquisition unit is used for acquiring working parameters of the unmanned aerial vehicle control device, wherein the working parameters comprise position information of the unmanned aerial vehicle control device, direction information of an antenna, pointing angle information of the antenna and transmitting power information of the interference signal; the first calculation unit is used for determining the relative position relation of each aircraft relative to the unmanned aerial vehicle control device according to the position information of the unmanned aerial vehicle control device and the position information of the multiple aircraft; and the second calculation unit is used for determining the interference intensity of the interference signal to each aircraft according to the direction information, the pointing angle information, the transmitting power information and the relative position relationship.

7. The airborne drone counteraction system of claim 6, wherein: the information acquisition module comprises a first data acquisition unit, a decoding unit and a second data acquisition unit; the first data acquisition unit is used for acquiring ADS-B data information of the aircraft in the current target control area; receiving ADS-B data information sent by an aircraft in the current target control area, or acquiring the ADS-B data information in the current target control area from first specified equipment; the decoding unit is used for decoding the ADS-B data information and determining the position information of a plurality of legal aircrafts in the current target control area; the second data acquisition unit is used for acquiring the position information of a plurality of legal aircrafts in the current target control area from second specified equipment.

8. The airborne drone counteraction system of claim 1, wherein: the unmanned aerial vehicle still includes the camera, the treater with the camera is connected, the treater passes through the camera acquires image information, and will image information sends for the unmanned aerial vehicle ground satellite station.

9. The airborne drone counteraction system of claim 1, wherein: the unmanned aerial vehicle is provided with a remote control receiving module; the remote control receiving module is used for receiving a remote control signal of the unmanned aerial vehicle ground station.

10. The airborne drone counteraction system of claim 1, wherein: the unmanned aerial vehicle ground station is a desktop computer, a notebook computer or a mobile terminal.

Technical Field

The invention relates to the technical field of radio interference, in particular to an airborne unmanned aerial vehicle counter-braking system.

Background

An unmanned aerial vehicle is a flying body that flies by remote control without a human being riding or that flies from the main along a specified route, and has been mainly used for military use in the past; because the consumption-level unmanned aerial vehicle is low in cost, easy to obtain and simple to control, and enters the market along with numerous unmanned aerial vehicle manufacturers, the commercial unmanned aerial vehicle can quickly go deep into the civil field, the number of users is gradually increased, the supervision difficulty is high, the commercial unmanned aerial vehicle can be easily utilized by lawbreakers, and if some lawbreakers use the unmanned aerial vehicle to steal and spy commercial secrets and the like, great pressure is brought to security and confidential work. In the international field, relevant precautionary measures have been taken for the black flying phenomenon of the unmanned aerial vehicle, however, the supervision of the domestic unmanned aerial vehicle is still in a blank state, and if corresponding precautionary control measures are not taken, the illegal unmanned aerial vehicle can cause great hidden troubles for aerial supervision and aerial safety; so that the anti-unmanned aerial vehicle technology is also in urgent need of development. Unmanned aerial vehicle's on the existing market survey and counter-braking equipment all set up on ground or car, are sheltered from by the building easily. Moreover, the existing unmanned aerial vehicle adopts a signal interference mode to perform countermeasures, and the arrangement is easy to influence nearby communication equipment on the ground, so that the effect is poor in an area with complex terrain and more shelters or an area which cannot interfere with the communication equipment.

Disclosure of Invention

The invention aims to overcome the defects of the prior art and provides an unmanned aerial vehicle with a counter-braking device and an unmanned aerial vehicle counter-braking system.

The invention is realized by the following technical scheme:

an airborne unmanned aerial vehicle control system comprises unmanned aerial vehicle control equipment, an unmanned aerial vehicle and an unmanned aerial vehicle ground station; the unmanned aerial vehicle counter-braking equipment is arranged inside the unmanned aerial vehicle; the unmanned aerial vehicle control device comprises a positioning module, a control module and a power module; the unmanned aerial vehicle is internally provided with a detection device and a processor; the unmanned aerial vehicle control device and the detection device are respectively in communication connection with the processor; the detection equipment is provided with a signal receiver and a signal processing circuit, and receives signals of the unmanned aerial vehicle ground station through the signal receiver; processing the signal of the ground station of the unmanned aerial vehicle through the signal processing circuit; the processor is used for receiving the reverse control data and sending an instruction for reversing the designated unmanned aerial vehicle to the reverse control module; the control module is provided with an unmanned aerial vehicle control circuit, and after receiving an instruction for controlling a designated unmanned aerial vehicle, the control module performs unmanned aerial vehicle control operation on the designated unmanned aerial vehicle through the unmanned aerial vehicle control circuit; the processor is connected with an unmanned aerial vehicle link of the unmanned aerial vehicle, and the unmanned aerial vehicle link transmits detection information sent by the detection equipment and the control data of the control equipment to the unmanned aerial vehicle ground station.

Further, the counter module comprises a signal generating unit, a power amplifying unit and a signal transmitting unit; the signal transmitting unit is connected with the power amplifying unit; the signal generation unit is respectively connected with the control module, the power supply module and the power amplification unit.

Further, the power supply module is electrically connected with a power supply device of the unmanned aerial vehicle; the power module is respectively and electrically connected with the positioning module, the control module and the counter module.

Furthermore, the unmanned aerial vehicle is provided with anti-interference equipment; the anti-interference navigation equipment comprises an information acquisition module, a calculation module and an anti-interference control module; the information acquisition module is used for acquiring the position information of a plurality of legal aircrafts in the current target control area in real time; the calculation module is used for determining the interference intensity of an interference signal sent by the unmanned aerial vehicle control device on each aircraft according to the position information of the plurality of aircraft and the working parameters of the unmanned aerial vehicle control device; and if the interference intensity of at least one target aircraft in the plurality of aircraft exceeds a preset interference intensity threshold value, the anti-interference control module controls the counter module to execute preset operation.

Further, the preset operation is a predefined operation for reducing the interference strength; the preset operation comprises controlling the unmanned aerial vehicle reverse braking equipment to stop sending out interference signals.

Further, the calculation module comprises a parameter acquisition unit, a first calculation unit and a second calculation unit; the parameter acquisition unit is used for acquiring working parameters of the unmanned aerial vehicle control device, wherein the working parameters comprise position information of the unmanned aerial vehicle control device, direction information of an antenna, pointing angle information of the antenna and transmitting power information of the interference signal; the first calculation unit is used for determining the relative position relation of each aircraft relative to the unmanned aerial vehicle control device according to the position information of the unmanned aerial vehicle control device and the position information of the multiple aircraft; and the second calculation unit is used for determining the interference intensity of the interference signal to each aircraft according to the direction information, the pointing angle information, the transmitting power information and the relative position relationship.

Further, the information acquisition module comprises a first data acquisition unit, a decoding unit and a second data acquisition unit; the first data acquisition unit is used for acquiring ADS-B data information of the aircraft in the current target control area; receiving ADS-B data information sent by an aircraft in the current target control area, or acquiring the ADS-B data information in the current target control area from first specified equipment; the decoding unit is used for decoding the ADS-B data information and determining the position information of a plurality of legal aircrafts in the current target control area; the second data acquisition unit is used for acquiring the position information of a plurality of legal aircrafts in the current target control area from second specified equipment.

Further, unmanned aerial vehicle still includes the camera, the treater with the camera is connected, the treater passes through the camera acquires image information, and will image information sends for unmanned aerial vehicle ground satellite station.

Further, the unmanned aerial vehicle is provided with a remote control receiving module; the remote control receiving module is used for receiving a remote control signal of the unmanned aerial vehicle ground station.

Further, the unmanned aerial vehicle ground station is a desktop computer, a notebook computer or a mobile terminal.

The invention has the beneficial effects that:

according to the airborne unmanned aerial vehicle anti-braking system, due to the fact that an electromagnetic interference mechanism is used, signal transmission between a remote control machine and an unmanned aerial vehicle is effectively interfered and cut off, signal transmission between the unmanned aerial vehicle and a remote control system and a navigation system of the unmanned aerial vehicle can be effectively interfered, portable anti-braking equipment of the unmanned aerial vehicle is small in size and light in weight, and is operated by a single person in a portable mode, and a positioning module returns the position of the anti-braking equipment in real time; the blocking frequency is accurate, a large-capacity storage battery is arranged in the device, the standby for an ultra-long time is guaranteed, and the device is not restricted by any terrain environment; the operation is simple, the operation can be carried out when the machine is started, the professional skill is not needed, the remote control module is arranged, the operation of remotely controlling the reverse control module can be realized, the reverse control equipment is fixed at a place where a person is inconvenient to approach, and the remote control module can be used for operation to realize reverse control striking; can stop wantonly in ground and the aerial position that the anti-system task needs, effectively solve the problem of the region space restriction that unmanned aerial vehicle anti-system equipment used, improve equipment greatly flexibility and rate of utilization.

Drawings

Fig. 1 is a schematic structural diagram of an airborne drone countermeasure system of an embodiment of the invention;

fig. 2 is a schematic structural diagram of an unmanned aerial vehicle ground station of an embodiment of the invention;

fig. 3 is a structural framework diagram of an airborne drone countermeasure system of an embodiment of the invention;

FIG. 4 is a structural framework diagram of a reverse module of an embodiment of the present invention;

fig. 5 is a structural framework diagram of the anti-interference apparatus of the embodiment of the present invention.

Detailed Description

The invention will be described in detail with reference to the drawings and specific embodiments, which are illustrative of the invention and are not to be construed as limiting the invention.

It should be noted that all the directional indications (such as up, down, left, right, front, back, upper end, lower end, top, bottom … …) in the embodiments of the present invention are only used to explain the relative position relationship between the components, the movement situation, etc. in a specific posture (as shown in the drawings), and if the specific posture is changed, the directional indication is changed accordingly.

In the present invention, unless expressly stated or limited otherwise, the term "coupled" is to be interpreted broadly, e.g., "coupled" may be fixedly coupled, detachably coupled, or integrally formed; can be mechanically or electrically connected; they may be directly connected or indirectly connected through intervening media, or they may be connected internally or in any other suitable relationship, unless expressly stated otherwise. The specific meanings of the above terms in the present invention can be understood by those skilled in the art according to specific situations.

In addition, the descriptions related to "first", "second", etc. in the present invention are only for descriptive purposes and are not to be construed as indicating or implying relative importance or implicitly indicating the number of technical features indicated. Thus, a feature defined as "first" or "second" may explicitly or implicitly include at least one such feature; in addition, technical solutions between various embodiments may be combined with each other, but must be realized by a person skilled in the art, and when the technical solutions are contradictory or cannot be realized, such a combination should not be considered to exist, and is not within the protection scope of the present invention.

Referring to fig. 1 to 5, an airborne drone countering system includes a drone countering device 2, a drone 1, and a drone ground station 3; the unmanned aerial vehicle control device 2 is arranged inside the unmanned aerial vehicle 1; the unmanned aerial vehicle reverse control equipment 2 comprises a positioning module, a control module, a reverse control module and a power supply module; the unmanned aerial vehicle 1 is internally provided with a detection device and a processor; the unmanned aerial vehicle control device 2 and the detection device are respectively in communication connection with the processor; the detection equipment is provided with a signal receiver and a signal processing circuit, and receives the signal of the unmanned aerial vehicle ground station 3 through the signal receiver; the signal processing circuit is used for processing the signal of the unmanned aerial vehicle ground station 3; the processor is used for receiving the reverse control data and sending an instruction for reversing the designated unmanned aerial vehicle to the reverse control module; the control module is provided with an unmanned aerial vehicle control circuit, and after receiving an instruction for controlling a designated unmanned aerial vehicle, the control module performs unmanned aerial vehicle control operation on the designated unmanned aerial vehicle through the unmanned aerial vehicle control circuit; the processor is connected with the unmanned aerial vehicle link of the unmanned aerial vehicle, and the unmanned aerial vehicle link transmits the detection information sent by the detection equipment and the control data of the control equipment to the unmanned aerial vehicle ground station 3.

It should be noted that, unmanned aerial vehicle counter-control equipment 2 suppresses the signal communication between unmanned aerial vehicle and remote controller, the GNSS through the wireless electromagnetic interference signal of the preset frequency channel of selection transmission, selects through control module to strike the frequency channel, and interference module suppresses the signal transmission who blocks unmanned aerial vehicle and remote controller, GNSS with transmission sub-frequency channel radio wave. By adopting the current advanced interference technology, the interference of flight control signals and navigation signals is specially processed, so that the excellent interference effect is achieved, the interference distance is far (the interference distance is more than 2 kilometers), the radiation is low, the device is light and convenient, and the device is simple to use and is portable by a single person. Control the portable control end of countering the system equipment of unmanned aerial vehicle, convey the unmanned aerial vehicle position and issue the observation that strikes the instruction and combine the people's eyes through the commander and confirm the unmanned aerial vehicle position, if some places are that personnel are inconvenient to be close to in the simultaneous control process, the remote controller can remote control countering the system module and open the place that is inconvenient to be close to at personnel to can counter the system through the remote control after will countering the system equipment and fix.

The portable anti-braking equipment of the unmanned aerial vehicle has small volume and light weight, is operated by a single person in a portable manner, and the positioning module returns the position of the anti-braking equipment in real time; the blocking frequency is accurate, a large-capacity storage battery is arranged in the device, the standby for an ultra-long time is guaranteed, and the device is not restricted by any terrain environment; the remote control device is simple to operate, can work when being started, does not need professional skills, can realize remote control of the operation of the reverse control module due to the arrangement of the remote control module, fixes the reverse control equipment at a place where a person is inconvenient to approach, can operate by using the remote control module, and realizes reverse control striking.

It should be noted that the detection device may be at least one of a radar, a radio frequency spectrum detection device, a photoelectric detection device, a sound wave detection device, and a television broadcast detection device. The processor can be STM32 series singlechip, atom treater, Snapdragon chip and other can use the main control chip on unmanned aerial vehicle, does not do the restriction here.

It should be noted that, the unmanned aerial vehicle that sets up detection equipment is when predetermineeing airspace flight, receives the electromagnetic wave signal and the sound wave signal that the external world sent through signal receiver, and signal processing circuit handles this signal in order to acquire probably adulterated unmanned aerial vehicle signal in this signal, according to this unmanned aerial vehicle signal identification unmanned aerial vehicle to the realization is through detection equipment detection unmanned aerial vehicle. The unmanned aerial vehicle can confirm all detected unmanned aerial vehicles as the designated unmanned aerial vehicle and send the information of the unmanned aerial vehicle, such as position information, communication frequency and the like to the processor; the detection device can also set the unmanned aerial vehicle detected in the preset time period as the designated unmanned aerial vehicle, or confirm the unmanned aerial vehicle of which the communication frequency is not the preset frequency and the preset instruction is not sent as the designated unmanned aerial vehicle.

It should be noted that, after the treater confirms that appointed unmanned aerial vehicle appears, carry out the counter-control to appointed unmanned aerial vehicle through the equipment of counter-controlling, wherein the mode of the appointed unmanned aerial vehicle of reflection equipment counter-control can be for interfering with unmanned aerial vehicle positioning system or controlling radio signal, and after unmanned aerial vehicle's signal or positioning system are disturbed, unmanned aerial vehicle automatic out of control forces to land, hover or return. The GPS positioning signal of the unmanned aerial vehicle can also be designated for interference, and the control signal interference can also be used. The interference mode of the control signal is divided into remote control signal frequency band blocking interference and tracking interference. The tracking interference can interfere specific to a specific frequency band according to the hopping of the remote control signal of the unmanned aerial vehicle, the interference range is reduced, the interference power is saved, and the influence on the electromagnetic environment is small.

Specifically, in this embodiment, the reverse module includes a signal generating unit, a power amplifying unit, and a signal transmitting unit; the signal transmitting unit is connected with the power amplifying unit; the signal generation unit is respectively connected with the control module, the power supply module and the power amplification unit.

Specifically, in this embodiment, the power module is electrically connected to a power supply device of the unmanned aerial vehicle; the power module is respectively and electrically connected with the positioning module, the control module and the counter module.

Specifically, in the scheme of this embodiment, the unmanned aerial vehicle is provided with an anti-interference device; the anti-interference navigation equipment comprises an information acquisition module, a calculation module and an anti-interference control module; the information acquisition module is used for acquiring the position information of a plurality of legal aircrafts in the current target control area in real time; the calculation module is used for determining the interference strength of the interference signal sent by the unmanned aerial vehicle control device 2 on each aircraft according to the position information of the plurality of aircraft and the working parameters of the unmanned aerial vehicle control device 2; and if the interference intensity of at least one target aircraft in the plurality of aircraft exceeds a preset interference intensity threshold value, the anti-interference control module controls the counter module to execute preset operation. It should be noted that the ADS-B data information acquired by directly receiving from the aircraft may include ADS-B data information that may include an illegal unmanned aerial vehicle, and therefore, after decoding the ADS-B data information, it is necessary to exclude the illegal unmanned aerial vehicle or determine a legal aircraft. Specifically, the judgment can be performed through the aircraft identity information obtained through decoding, and if the corresponding aircraft is allowed to enter the current target monitoring area through a relevant supervision department according to the aircraft identity information, the aircraft can be considered to be a legal flight. The working parameters comprise position information of the unmanned aerial vehicle counter-braking device 2, direction information of the antenna, pointing angle information of the antenna and transmitting power information of the interference signal.

It should be noted that the interference strength threshold may be understood as any preset threshold, for example, a safety threshold when a legal aircraft receives satellite positioning signals and is interfered, and if the safety threshold is exceeded, the aircraft may have a problem of inaccurate positioning. The interference intensity threshold corresponds to the interference intensity, and if the radiation intensity of the interference signal radiated to the current position of the aircraft is taken as a judgment basis, the interference intensity threshold represents the signal intensity; if the signal-to-noise ratio of the satellite positioning signal received by the aircraft is taken as a judgment basis, the interference intensity threshold value represents the signal-to-noise ratio of the received satellite positioning signal. And adjusting adjustable parameters in the working parameters of the unmanned aerial vehicle control device 2. The adjustable parameter may be understood as a working parameter capable of being dynamically adjusted, and since the working parameter is associated with the coverage area of the interference signal and the distribution manner of the signal strength of the interference signal, the coverage area of the interference signal and the distribution manner of the signal strength of the interference signal may be affected by adjusting the working parameter.

Specifically, in this embodiment, the preset operation is a predefined operation for reducing the interference strength; the preset operation comprises controlling the unmanned aerial vehicle counter-braking device 2 to stop sending the interference signal.

Specifically, in this embodiment, the calculation module includes a parameter obtaining unit, a first calculation unit, and a second calculation unit; the parameter acquiring unit is used for acquiring working parameters of the unmanned aerial vehicle control device 2, wherein the working parameters comprise position information of the unmanned aerial vehicle control device 2, direction information of an antenna, pointing angle information of the antenna and transmitting power information of the interference signal; the first calculation unit is used for determining the relative position relation of each aircraft relative to the unmanned aerial vehicle control device 2 according to the position information of the unmanned aerial vehicle control device 2 and the position information of a plurality of aircraft; and the second calculation unit is used for determining the interference intensity of the interference signal to each aircraft according to the direction information, the pointing angle information, the transmitting power information and the relative position relationship.

Specifically, in this embodiment, the information obtaining module includes a first data obtaining unit, a decoding unit, and a second data obtaining unit; the first data acquisition unit is used for acquiring ADS-B data information of the aircraft in the current target control area; receiving ADS-B data information sent by an aircraft in the current target control area, or acquiring the ADS-B data information in the current target control area from first specified equipment; the decoding unit is used for decoding the ADS-B data information and determining the position information of a plurality of legal aircrafts in the current target control area; the second data acquisition unit is used for acquiring the position information of a plurality of legal aircrafts in the current target control area from second specified equipment. It should be noted that ADS-B specifically refers to: automatic Dependent Surveillance-Broadcast, which can be understood as Broadcast auto correlation monitoring. The ADS-B data information of the aircraft includes flight status information of the aircraft, and specifically may include: location information of the aircraft, altitude information, speed information, heading information, aircraft identity information (e.g., identification number), etc. According to the anti-interference device of the unmanned aerial vehicle anti-braking equipment 2, after the position information of the legal aircraft in the current target control area is obtained in real time, the interference degree of the satellite positioning signal receiving capacity of the corresponding aircraft by the interference signal is determined, if the interference intensity of the aircraft exceeds the preset interference intensity threshold value, the unmanned aerial vehicle anti-braking equipment 2 is controlled to execute the operation for reducing the interference intensity, so that the indication and the control of whether the unmanned aerial vehicle anti-braking equipment interferes with the flight of the legal aircraft can be made, the unmanned aerial vehicle anti-braking is considered, and the interference on the normal flight is avoided.

Specifically, in this embodiment, unmanned aerial vehicle still includes the camera, the treater with the camera is connected, the treater passes through the camera acquires image information, and will image information sends for unmanned aerial vehicle ground satellite station 3.

Specifically, in this embodiment, the unmanned aerial vehicle is provided with a remote control receiving module; the remote control receiving module is used for receiving a remote control signal of the unmanned aerial vehicle ground station 3.

Specifically, in this embodiment, the ground station 3 of the unmanned aerial vehicle is a desktop computer, a notebook computer or a mobile terminal.

The technical solutions provided by the embodiments of the present invention are described in detail above, and the principles and embodiments of the present invention are explained herein by using specific examples, and the descriptions of the embodiments are only used to help understanding the principles of the embodiments of the present invention; meanwhile, for a person skilled in the art, according to the embodiments of the present invention, there may be variations in the specific implementation manners and application ranges, and in summary, the content of the present description should not be construed as a limitation to the present invention.