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Formation Control Method of Aeronautical Missile Swarm System Based on Consistency Theory

A technology of swarm system and control method, which is applied in the field of formation control for the swarm system of flying missiles, can solve the problems of control accuracy, model complexity and algorithm complexity, and is difficult to coordinate, and achieve the effect of simple control law and easy execution

Active Publication Date: 2022-01-11
BEIJING RES INST OF MECHANICAL & ELECTRICAL TECH
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Problems solved by technology

[0008] Aiming at the technical problems that are difficult to coordinate in terms of control accuracy, model complexity, and algorithm complexity in the formation control of the aerial missile swarm system in the prior art, the present invention provides a formation control method for the aerial missile swarm system based on the consistency theory

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  • Formation Control Method of Aeronautical Missile Swarm System Based on Consistency Theory
  • Formation Control Method of Aeronautical Missile Swarm System Based on Consistency Theory
  • Formation Control Method of Aeronautical Missile Swarm System Based on Consistency Theory

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Embodiment Construction

[0043] The basic idea of ​​a consensus-based formation control strategy is that the states or outputs of all monomers in a swarm system maintain a specific deviation with respect to a common formation reference. At the beginning of the formation, the formation reference remains unknown to the monomers. After distributed cooperative control, all monomers reach an agreement on the formation reference, and then realize the desired formation.

[0044] In view of the advantages of the consensus-based formation control strategy in the distributed cooperative control of the cluster system, the present invention proposes a collaborative control method based on the consistency theory for the aircraft missile cluster system, and designs the guidance loop to generate the formation of the aircraft missile cluster system Expected acceleration, design the control loop to control the missile unit to track the corresponding acceleration, such as figure 1shown. The guidance loop pre-stores th...

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Abstract

The present invention provides a formation control method of the aerial missile swarm system based on the consistency theory. First, the topological structure parameters of the aerial missile swarm system, the position information of the cells, the formation reference information, and the relative speed of the adjacent cells are obtained; The formation control law in the guidance loop is calculated based on the consistency theory, and the formation control law is used as the expected acceleration of acceleration tracking in the control loop; finally, the expected acceleration is decomposed into the x-direction and z-direction expected acceleration of the velocity system, and the engine throttle, speed The inclination angle is the actuator of the flying missile, and the PI control is used to track the acceleration in the x and z directions, and the formation control of the flying missile cluster system is realized by controlling the acceleration of the missile to track the expected acceleration. The formation control method has the characteristics of fully distributed computing, low resource occupancy, high control precision, and easy algorithm implementation, and has good practicability.

Description

technical field [0001] The invention relates to the technical field of missile formation control, in particular to a formation control method aimed at a flight missile cluster system. Background technique [0002] A cluster system is a system composed of a large number of autonomous or semi-autonomous subjects that are distributed and configured through the network interconnection. For missile weapon systems, cluster coordination can promote the development of missiles from relatively simple single-bomb functions to more complex cluster cooperative operations. The missile cluster system can disperse the various functions of a single complex combat platform into a large number of low-level In the micro-element missile with single cost and function, the original complex system function is realized through a large number of heterogeneous and heterogeneous individuals, and the multiplication benefit of the system will enable the missile cluster to have a combat capability far ex...

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G05D1/10
CPCG05D1/107
Inventor 徐星光杨保华魏振岩马跃
Owner BEIJING RES INST OF MECHANICAL & ELECTRICAL TECH
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