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Formation control method for multi-quadrotor aircraft containing predictor

A technology of quadrotor aircraft and control method, which is applied in attitude control, comprehensive factory control, control/regulation system, etc., and can solve the problems that quadrotor aircraft research has not made great progress

Active Publication Date: 2021-01-15
NANJING UNIV OF POSTS & TELECOMM
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, due to the limitation of generator volume and other aspects, until the 1990s, the research of quadrotor aircraft did not make great progress.

Method used

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  • Formation control method for multi-quadrotor aircraft containing predictor
  • Formation control method for multi-quadrotor aircraft containing predictor
  • Formation control method for multi-quadrotor aircraft containing predictor

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Effect test

Embodiment Construction

[0080] Attached below Figure 1-2 The technical scheme of the present invention is described in further detail:

[0081] The present invention proposes a kind of formation control method that contains the multi-quadrotor aircraft of predictor, comprises the following steps:

[0082] Step 1, set a quadrotor aircraft as the leader, set N quadrotor aircraft with unknown dynamics as followers, and the networked system connected by followers and leaders through a one-way topological graph as the controlled object;

[0083] Step 2, the i-th follower among the N followers is equipped with a position controller and an attitude controller, and the input terminals of the position controller and attitude controller of the i-th follower are connected with the directed graph The output of the i-th follower's position controller is connected to the input of its position controller, the output of the i-th follower's attitude controller is connected to the input of the i-th follower's attit...

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PUM

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Abstract

The invention provides a formation control method for a multi-quadrotor aircraft with a predictor. The method comprises the following steps: 1, setting one quadrotor aircraft as a leader, setting N quadrotor aircrafts with unknown dynamics as followers, and enabling a networked system formed by the followers and the leader through the connection of a one-way topological graph to serve as a controlled object; and 2, arranging a position controller and a posture controller on the ith follower in the N followers, connecting the input end of the position controller and the input end of the posturecontroller of the ith follower with the output end of a directed graph G, connecting the output end of the position controller of the ith follower is connected with the input end of the position controller of the ith follower, and connecting the output end of the ith follower posture controller with the input end of the posture controller of the ith follower. Collision avoidance and connection maintenance among the multi-quadrotor aircrafts are realized, an expected formation pattern is completed, obstacles are avoided, and a formation control target is completed in a predetermined performance range.

Description

technical field [0001] The invention relates to the design of a multi-quadrotor aircraft formation collision avoidance controller including an predictor, and belongs to the technical field of industrial process control. Background technique [0002] In recent years, due to its small size and light weight, the quadrotor aircraft is very suitable for tasks such as near-ground reconnaissance, surveillance, aerial photography, and agricultural sowing, and has been widely used in military and civilian applications. However, the four-rotor aircraft has a history of one hundred years of development. As early as 1907, the world's first four-rotor helicopter was manufactured by the French Breguet brother Louis. Etienne Oemichen, a French engineer at Peugeot, designed the first quadrotor capable of hovering in history in 1924. In 1956, the American designer Convertawing built a quadrotor aircraft using two engines, and the attitude of the aircraft was controlled by changing the speed...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G05D1/08
CPCG05D1/0833Y02P90/02
Inventor 杨杨刘奇东陈笛笛岳东张腾飞赵勃
Owner NANJING UNIV OF POSTS & TELECOMM
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