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Cooperative guidance method based on leader and follower principle

A follower and leader technology, applied in the control/regulation system, non-electric variable control, three-dimensional position/course control, etc., can solve the problems of reaching the target position, unable to fly the aircraft group, etc., and achieve a stable flight path and system stability Good, the effect of simplifying the control process

Active Publication Date: 2021-07-16
BEIJING INSTITUTE OF TECHNOLOGYGY
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] In addition, sometimes the target that the aircraft group needs to approach is in a moving state, and the established guidance law will not allow the aircraft group to reach the moving target position

Method used

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  • Cooperative guidance method based on leader and follower principle
  • Cooperative guidance method based on leader and follower principle
  • Cooperative guidance method based on leader and follower principle

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0121] The simulation experiment is set as follows: three aircraft form a cooperative guidance system, one of which is the pilot aircraft, and two of them are follower aircraft. Fly horizontally in the negative direction of the x-axis, the initial velocity of the pilot aircraft is 200m / s, and the initial line-of-sight angle is 45°. The initial position of the leading aircraft is 0, the value of the position vector L between the predetermined position of the following aircraft and the leading aircraft is 100m,

[0122] During the flight, the distance between the following aircraft and the leading aircraft is always 100±10m, and the positional relationship between the aircraft at the guidance terminal and the target is:

[0123] location information Target follow aircraft 1 pilot aircraft follow the aircraft 2 Horizontal position / m 1966.43 2063.52 1964.56 1866.28 Vertical position / m 2828.43 2825.27 2826.42 2824.42

[0124] Simulation resu...

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PUM

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Abstract

The invention discloses a cooperative guidance method and system based on a leader and follower principle. A piloting aircraft and a following aircraft are arranged, the piloting aircraft carries out guidance, the following aircraft follows the piloting aircraft to achieve cooperative guidance, and the piloting aircraft obtains guidance parameters by constructing a neural network in the guidance process. The cooperative guidance method and system based on the leader and follower principle have the advantages that the control process of the multiple aircrafts during guidance is simplified, the flight path is stable and efficient in the guidance process, and the system stability is good.

Description

technical field [0001] The invention relates to a guidance method, in particular to a cooperative guidance method based on the leader-follower principle, which belongs to the field of unmanned aerial vehicle control. Background technique [0002] Nowadays, unmanned aerial vehicles have been widely used in engineering practice. During the cluster flight of the aircraft, it needs to be controlled cooperatively. [0003] However, when multiple aircraft form an aircraft group for long-distance flight (intermediate guidance), due to the need for simultaneous control of guidance, attitude, and aircraft coordination, the amount of calculation will increase significantly, which requires a relatively simple and efficient coordination Guidance method is used to guide multi-vehicles for long-distance formation flight. [0004] In addition, sometimes the target that the aircraft group needs to approach is in a moving state, and the established guidance law will not allow the aircraft ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G05D1/10
CPCG05D1/104
Inventor 刘佳琪王伟林德福王江王辉林时尧
Owner BEIJING INSTITUTE OF TECHNOLOGYGY
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