Aerodynamic missile cluster system formation control method 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: 2019-08-23
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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  • Aerodynamic missile cluster system formation control method based on consistency theory
  • Aerodynamic missile cluster system formation control method based on consistency theory
  • Aerodynamic missile cluster system formation control method 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 invention provides an aerodynamic missile cluster system formation control method based on a consistency theory. Firstly, topology structure parameters, single position information, formation reference information and relative speed of adjacent single bodies of an aerodynamic missile cluster system are obtained; then, a formation control law in a guidance loop is calculated based on the consistency theory and the formation control law is used as expected acceleration of acceleration tracking in a control loop; and finally, the expected acceleration is decomposed into x-direction and Z-direction expected acceleration of a speed system, an engine throttle and a speed inclination angle are used as an aerodynamic missile execution mechanism, and PI control is used to track the x-directionand Z-direction acceleration, and missile acceleration is controlled to track the expected acceleration to control a formation of the aerodynamic missile cluster system. The formation control method has the characteristics of single fully distributed computing, low resource occupancy, high control precision and easy implementation of algorithm, 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 Applications(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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