A Fully Distributed Robust Missile Formation Cooperative Controller

Abstract

The invention discloses a fully distributed robust missile formation cooperative controller, which consists of a fully distributed adaptive controller (100), an adaptive compensation controller (200), a control command fusion module (300) and a missile dynamic model (400) composition. The control instruction fusion module (300) sums the fully distributed control instruction and the compensation control instruction to obtain the motion control input instruction u i The missile dynamic model (400) is designed for three-dimensional space particles; the parameters required by the controller of the present invention have nothing to do with the overall information of the communication topology, and do not need the structural information of the communication structure diagram, and it only depends on the relative positions of the missile itself and its neighbor missiles and speed. In this way, the missile formation can achieve the technical effect of fully distributed formation stable flight and maintaining formation formation under various uncertain interference factors.

Description

technical field [0001] The present invention relates to the design of a missile formation controller, more particularly, the fully distributed robust missile formation cooperative controller designed by the present invention is added to the traditional missile autonomous formation cooperative guidance control system. Background technique [0002] A missile (Missile) usually consists of four parts: warhead (warhead), body structure system, power plant propulsion system and guidance system. Among them, the missile guidance system is a general term for various devices such as guiding the missile to the target according to a certain guiding law, controlling its movement around the center of mass and its movement around the center of mass, as well as the time-of-flight program, command signal, power supply, and power distribution. Its function is to timely measure the position of the missile relative to the target, determine the flight trajectory of the missile, control the fligh...

AI Technical Summary

Problems solved by technology

[0007] In order to solve the formation control of the missile formation in the process of large-scale maneuvering flight, and the task that the formation formation cannot be kept stable due to uncertain factors and external environmental interference factors, the present invention designs a completely distributed robust missile formation cooperative controller

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