阅读说明：本技术 一种直升机电传操纵系统位移传感器布置方法 (Method for arranging displacement sensors of fly-by-wire control system of helicopter ) 是由 孙冲 邓海侠 张根源 于 2019-12-04 设计创作，主要内容包括：本发明属于直升机电传操纵领域,具体涉及一种直升机电传操纵系统位移传感器布置方法。该方法包括：根据通道耦合情况对各个通道布置N个位移传感器；针对每个通道使驾驶员操纵杆移动预定位移同时采集位移传感器的输入角度；确定驾驶员操纵杆位移与N个位移传感器的输入角度的关系曲线；分别针对每个通道对比N个关系曲线中的任意两条曲线的斜率的差值；针对每个通道在任意两条曲线的斜率的差值大于要求值的情况下,更改位移传感器连接拉杆长度或驾驶杆到位移传感器的传动比,直到任意两条曲线的斜率的差值不大于要求值。该方法提高了指令传感器输出信号的准确性,避免了多余度位移传感器输出差异过大而影响故障判别的问题。(The invention belongs to the field of fly-by-wire operation of helicopters, and particularly relates to a method for arranging displacement sensors of a fly-by-wire operation system of a helicopter. The method comprises the following steps: arranging N displacement sensors for each channel according to the channel coupling condition; moving a driver joystick by a predetermined displacement for each channel while acquiring an input angle of a displacement sensor; determining a relation curve of the displacement of the control lever of the driver and the input angle of the N displacement sensors; respectively comparing the difference values of the slopes of any two curves in the N relation curves aiming at each channel; and under the condition that the difference of the slopes of any two curves of each channel is greater than the required value, changing the length of a connecting pull rod of the displacement sensor or the transmission ratio of the steering column to the displacement sensor until the difference of the slopes of any two curves is not greater than the required value. The method improves the accuracy of the output signal of the command sensor and avoids the problem that the output difference of the redundancy displacement sensor is too large to influence the fault judgment.)

1. A method for arranging displacement sensors of a fly-by-wire helicopter control system is characterized by comprising the following steps:

arranging N displacement sensors for each channel according to the channel coupling condition, wherein N is an integer greater than or equal to 2;

moving a driver joystick by a predetermined displacement for each channel while acquiring an input angle of a displacement sensor;

respectively determining a relation curve of the displacement of the control lever of the driver and the input angle of the N displacement sensors for each channel;

respectively comparing the difference values of the slopes of any two curves in the N relation curves aiming at each channel;

and under the condition that the difference of the slopes of any two curves of each channel is greater than the required value, changing the length of a connecting pull rod of the displacement sensor or the transmission ratio of the steering column to the displacement sensor until the difference of the slopes of any two curves is not greater than the required value.

2. The method of claim 1, comprising: arranging N displacement sensors for each channel according to the channel coupling condition, specifically comprising:

under the condition that coupled channels do not exist, N displacement sensors are respectively and symmetrically distributed on each channel;

in the presence of coupled channels, N displacement sensors are respectively arranged on the coupled channels in a symmetrically distributed manner, and are connected with the control output pull rod, and N displacement sensors are respectively arranged on the uncoupled channels in a symmetrically distributed manner.

3. The method of claim 1, wherein moving the driver joystick a predetermined displacement for each channel while collecting input angles of the displacement sensors, specifically comprises:

under the condition that coupling does not exist, establishing a motion model of a control mechanism of the cockpit;

and simulating by using a motion model of the control mechanism of the cockpit, so that the control lever of the driver moves through the full stroke and simultaneously and synchronously acquires the input angle of the displacement sensor.

4. The method of claim 2, wherein moving the driver joystick a predetermined displacement for each channel while collecting the input angle of the displacement sensor, specifically comprises:

under the condition that coupling exists, establishing a motion model of a control mechanism of the cockpit;

and simulating by using a motion model of the control mechanism of the cockpit, so that the control lever of the driver moves in a full stroke and simultaneously and synchronously acquires the input angle of the non-coupling channel displacement sensor and the input angle of the coupling channel displacement sensor.

5. The method according to claim 3, wherein determining a driver joystick displacement versus input angle of N displacement sensors for each channel separately comprises:

in the case of no coupled channel, the driver joystick displacement is used as an abscissa, and the input angles of the N displacement sensors are used as ordinates to determine N relation curves.

6. The method according to claim 4, wherein determining a driver joystick displacement versus input angle of N displacement sensors for each channel separately comprises:

in the case where there are channels that are coupled,

determining N non-coupled channel relation curves by taking the displacement of a control lever of a driver as an abscissa and taking the input angles of N displacement sensors of the non-coupled channels as an ordinate;

and determining N coupling channel relation curves by taking the displacement of the control lever of the driver as an abscissa and respectively taking the input angles of the N displacement sensors of the coupled channels as an ordinate.

7. The method according to claim 5, wherein, in the case that the difference between the slopes of any two curves is greater than a required value for each channel, the step of changing the length of the connecting rod of the displacement sensor or the transmission ratio of the steering column to the displacement sensor until the difference between the slopes of any two curves is not greater than the required value comprises:

in the case of no coupled channel, if the difference between the slopes of any two curves of a certain channel is greater than the first required value, the length of the connecting pull rod of the displacement sensor of the channel or the transmission ratio of the steering column to the displacement sensor is changed until the difference between the slopes of any two curves of the channel is not greater than the first required value.

8. The method according to claim 6, wherein, in the case that the difference between the slopes of any two curves is greater than a required value for each channel, the step of changing the length of the connecting rod of the displacement sensor or the transmission ratio of the steering rod to the displacement sensor until the difference between the slopes of any two curves is not greater than the required value comprises:

under the condition that a coupled channel exists, if the difference value of the slopes of any two curves in the relation curves of the N coupled channels of the coupled channel is larger than a second required value, changing the length of the control output pull rod, the length of a connecting pull rod of the displacement sensor or the transmission ratio of the steering rod to the displacement sensor until the difference value of the slopes of any two curves is not larger than the second required value;

and if the difference value of the slopes of any two curves in the N non-coupled channel relation curves of the non-coupled channel is greater than the first required value, changing the length of a connecting pull rod of the displacement sensor of the channel or the transmission ratio of the steering column to the displacement sensor until the difference value of the slopes of any two curves of the channel is not greater than the first required value.

Technical Field

The invention belongs to the field of fly-by-wire operation of helicopters, and particularly relates to a method for arranging displacement sensors of a fly-by-wire operation system of a helicopter.

Background

The input instruction of a driver of the traditional control system is transmitted to a control surface through a mechanical lever system or a control steel cable, so that the pitch of a main propeller and a tail propeller of the helicopter is changed; the input instruction of a driver of the fly-by-wire control system is converted into an electric signal through a displacement sensor and transmitted to a flight control computer to drive the steering engine, so that the pitch of the blades is changed. Therefore, the command sensors required for the basic control loop are important components of the fly-by-wire system of the helicopter.

Based on the consideration of safety and reliability, each channel of the telex system is provided with a displacement sensor with mechanical redundancy serving as a backup. The difference of the output characteristics of the displacement sensors directly influences the identification and discrimination of the fly-by-wire control system on the signals of the displacement sensors of the channel, and the identification of faults of the fly-by-wire control system, namely the safety guarantee of the airplane, is influenced by overlarge difference.

Disclosure of Invention

The purpose of the invention is as follows: the method is used for arranging and analyzing the command sensor of the driver, improves the accuracy of the output signal of the command sensor, and avoids the problem that the fault discrimination is influenced by overlarge output difference of the redundancy displacement sensor.

The technical scheme of the invention is as follows:

in a first aspect, a helicopter fly-by-wire system displacement sensor arrangement method is provided, comprising:

arranging N displacement sensors for each channel according to the channel coupling condition, wherein N is an integer greater than or equal to 2;

moving a driver joystick by a predetermined displacement for each channel while acquiring an input angle of a displacement sensor;

respectively determining a relation curve of the displacement of the control lever of the driver and the input angle of the N displacement sensors for each channel;

respectively comparing the difference values of the slopes of any two curves in the N relation curves aiming at each channel;

and under the condition that the difference of the slopes of any two curves of each channel is greater than the required value, changing the length of a connecting pull rod of the displacement sensor or the transmission ratio of the steering column to the displacement sensor until the difference of the slopes of any two curves is not greater than the required value.

Optionally, comprising: arranging N displacement sensors for each channel according to the channel coupling condition, specifically comprising:

under the condition that coupled channels do not exist, N displacement sensors are respectively and symmetrically distributed on each channel;

in the presence of coupled channels, N displacement sensors are respectively arranged on the coupled channels in a symmetrically distributed manner, and are connected with the control output pull rod, and N displacement sensors are respectively arranged on the uncoupled channels in a symmetrically distributed manner.

Optionally, moving the driver joystick by a predetermined displacement for each channel while acquiring an input angle of the displacement sensor specifically includes:

under the condition that coupling does not exist, establishing a motion model of a control mechanism of the cockpit;

and simulating by using a motion model of the control mechanism of the cockpit, so that the control lever of the driver moves through the full stroke and simultaneously and synchronously acquires the input angle of the displacement sensor.

Optionally, moving the driver joystick by a predetermined displacement for each channel while acquiring an input angle of the displacement sensor specifically includes:

under the condition that coupling exists, establishing a motion model of a control mechanism of the cockpit;

and simulating by using a motion model of the control mechanism of the cockpit, so that the control lever of the driver moves in a full stroke and simultaneously and synchronously acquires the input angle of the non-coupling channel displacement sensor and the input angle of the coupling channel displacement sensor.

Optionally, determining a relationship curve of the driver joystick displacement and the input angle of the N displacement sensors for each channel respectively specifically includes:

in the absence of a coupled channel, N relationship curves are determined with the driver's joystick displacement as the abscissa and the input angles of the N displacement sensors as the ordinate, respectively.

Optionally, determining a relationship curve of the driver joystick displacement and the input angle of the N displacement sensors for each channel respectively specifically includes:

in the case where there are channels that are coupled,

determining N non-coupled channel relation curves by taking the displacement of a control lever of a driver as an abscissa and taking the input angles of N displacement sensors of the non-coupled channels as an ordinate;

and determining N coupling channel relation curves by taking the displacement of the control lever of the driver as an abscissa and respectively taking the input angles of the N displacement sensors of the coupled channels as an ordinate.

Optionally, in a case that a difference between slopes of any two curves of each channel is greater than a required value, changing a length of a tie rod connected to the displacement sensor or a transmission ratio of the steering column to the displacement sensor until the difference between the slopes of any two curves is not greater than the required value, specifically including:

in the case of no coupled channel, if the difference between the slopes of any two curves of a certain channel is greater than the first required value, the length of the connecting pull rod of the displacement sensor of the channel or the transmission ratio of the steering column to the displacement sensor is changed until the difference between the slopes of any two curves of the channel is not greater than the first required value.

Optionally, in a case that a difference between slopes of any two curves of each channel is greater than a required value, changing a length of a tie rod connected to the displacement sensor or a transmission ratio of the steering column to the displacement sensor until the difference between the slopes of any two curves is not greater than the required value, specifically including:

under the condition that a coupled channel exists, if the difference value of the slopes of any two curves in the relation curves of the N coupled channels of the coupled channel is larger than a second required value, changing the length of the control output pull rod, the length of a connecting pull rod of the displacement sensor or the transmission ratio of the steering rod to the displacement sensor until the difference value of the slopes of any two curves is not larger than the second required value;

and if the difference value of the slopes of any two curves in the N non-coupled channel relation curves of the non-coupled channel is greater than the first required value, changing the length of a connecting pull rod of the displacement sensor of the channel or the transmission ratio of the steering column to the displacement sensor until the difference value of the slopes of any two curves of the channel is not greater than the first required value.

The invention has the beneficial effects that: the method for analyzing the layout of the displacement sensors of the fly-by-wire helicopter control system can be well applied to the overall layout design of the displacement sensors of the helicopter, is accurate, efficient and easy to operate, can improve the signal consistency of mechanical redundancy displacement sensors, and avoids the problem of system fault discrimination.

Drawings

Fig. 1 is a flow chart of a method for arranging displacement sensors of a fly-by-wire helicopter control system according to an embodiment of the present invention.

Detailed Description

The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.

The invention discloses a method for arranging displacement sensors of a fly-by-wire helicopter control system, which comprises the following steps: arranging N displacement sensors for each channel according to the channel coupling condition, wherein N is an integer greater than or equal to 2; moving a driver joystick by a predetermined displacement for each channel while acquiring an input angle of a displacement sensor; respectively determining a relation curve of the displacement of the control lever of the driver and the input angle of the N displacement sensors for each channel; respectively comparing the difference values of the slopes of any two curves in the N relation curves aiming at each channel; and under the condition that the difference of the slopes of any two curves of each channel is greater than the required value, changing the length of a connecting pull rod of the displacement sensor or the transmission ratio of the steering column to the displacement sensor until the difference of the slopes of any two curves is not greater than the required value.

Optionally, comprising: arranging N displacement sensors for each channel according to the channel coupling condition, specifically comprising: under the condition that coupled channels do not exist, N displacement sensors are respectively and symmetrically distributed on each channel; in the presence of coupled channels, N displacement sensors are respectively arranged on the coupled channels in a symmetrically distributed manner, and are connected with the control output pull rod, and N displacement sensors are respectively arranged on the uncoupled channels in a symmetrically distributed manner.

Optionally, moving the driver joystick by a predetermined displacement for each channel while acquiring an input angle of the displacement sensor specifically includes: under the condition that coupling does not exist, establishing a motion model of a control mechanism of the cockpit; and simulating by using a motion model of the control mechanism of the cockpit, so that the control lever of the driver moves through the full stroke and simultaneously and synchronously acquires the input angle of the displacement sensor.

Optionally, moving the driver joystick by a predetermined displacement for each channel while acquiring an input angle of the displacement sensor specifically includes: under the condition that coupling exists, establishing a motion model of a control mechanism of the cockpit; and simulating by using a motion model of the control mechanism of the cockpit, so that the control lever of the driver moves in a full stroke and simultaneously and synchronously acquires the input angle of the non-coupling channel displacement sensor and the input angle of the coupling channel displacement sensor.

Optionally, determining a relationship curve of the driver joystick displacement and the input angle of the N displacement sensors for each channel respectively specifically includes: in the absence of a coupled channel, N relationship curves are determined with the driver's joystick displacement as the abscissa and the input angles of the N displacement sensors as the ordinate, respectively.

Optionally, determining a relationship curve of the driver joystick displacement and the input angle of the N displacement sensors for each channel respectively specifically includes: under the condition that a coupled channel exists, determining N non-coupled channel relation curves by taking the displacement of a control lever of a driver as an abscissa and respectively taking the input angles of N displacement sensors of the non-coupled channel as an ordinate; and determining N coupling channel relation curves by taking the displacement of the control lever of the driver as an abscissa and respectively taking the input angles of the N displacement sensors of the coupled channels as an ordinate.

Optionally, in a case that a difference between slopes of any two curves of each channel is greater than a required value, changing a length of a tie rod connected to the displacement sensor or a transmission ratio of the steering column to the displacement sensor until the difference between the slopes of any two curves is not greater than the required value, specifically including: in the case of no coupled channel, if the difference between the slopes of any two curves of a certain channel is greater than the first required value, the length of the connecting pull rod of the displacement sensor of the channel or the transmission ratio of the steering column to the displacement sensor is changed until the difference between the slopes of any two curves of the channel is not greater than the first required value.

Optionally, in a case that a difference between slopes of any two curves of each channel is greater than a required value, changing a length of a tie rod connected to the displacement sensor or a transmission ratio of the steering column to the displacement sensor until the difference between the slopes of any two curves is not greater than the required value, specifically including: under the condition that a coupled channel exists, if the difference value of the slopes of any two curves in the relation curves of the N coupled channels of the coupled channel is larger than a second required value, changing the length of the control output pull rod, the length of a connecting pull rod of the displacement sensor or the transmission ratio of the steering rod to the displacement sensor until the difference value of the slopes of any two curves is not larger than the second required value; and if the difference value of the slopes of any two curves in the N non-coupled channel relation curves of the non-coupled channel is greater than the first required value, changing the length of a connecting pull rod of the displacement sensor of the channel or the transmission ratio of the steering column to the displacement sensor until the difference value of the slopes of any two curves of the channel is not greater than the first required value.

The method for analyzing the layout of the displacement sensors of the fly-by-wire control system of the helicopter is mainly used for the layout and analysis of the command sensors of the driver, improves the accuracy of the output signals of the command sensors and avoids the problem that the output difference of redundant displacement sensors is too large to influence the fault judgment. The method is used for assisting the fly-by-wire system scheme design.

The arrangement principle is as follows: 1. the input consistency of each channel redundancy displacement sensor is ensured, the output difference of the redundancy displacement sensors is reduced, and the redundancy displacement sensors are ensured to be within the specified range of the design requirement; 2. the battlefield viability of the displacement sensor is improved, and the displacement sensor is symmetrically distributed.

The key points of the invention are as follows: 1. providing analysis basis for the arrangement of the displacement sensor; 2. modeling and analyzing a displacement sensor arrangement scheme by a motion mechanism; 3. reducing the influence of coupling on the signal consistency of the displacement sensor; 4. and the input consistency of the redundancy sensor in the channel is ensured.