航天控制2024,Vol.42Issue(6) :3-10.

无动力飞行器分布式有限时间编队跟踪控制

Distributed Finite-Time Formation Tracking Control of Unpowered Vehicles

生百世 禹春梅 王亮 梁禄扬
航天控制2024,Vol.42Issue(6) :3-10.

无动力飞行器分布式有限时间编队跟踪控制

Distributed Finite-Time Formation Tracking Control of Unpowered Vehicles

生百世 1禹春梅 1王亮 1梁禄扬1
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作者信息

  • 1. 北京航天自动控制研究所,北京 100854
  • 折叠

摘要

针对无动力飞行器再入过程中的编队控制问题,基于虚拟领导者的二阶系统一致性控制理论,优化了协调变量并引入过渡环节,提出了一种集结时间可调的分布式编队保持与切换控制算法.该算法结合飞行能力和编队任务需求,允许无动力飞行器的高程在一定范围内变化,在线实现对多无动力飞行器相对横程和相对纵程的精确控制.仿真结果表明,该算法在编队形成与保持、编队构型切换和编队横向规避场景下,均可实现对期望编队构型的精确控制,并且仿真过程还加入了地球曲率和自转效应对再入动力学的影响.算法同时能够适应偏差随机的气动系数和大气密度的组合拉偏,具有良好的鲁棒性.

Abstract

A method aiming at the formation control problem during the reentry of multi-unpowered vehicles is discussed in this paper.Based on second-order system consistency theory of virtual leader,a distributed formation keeping and control algorithm switching of adjustable assembly time is proposed by selecting opti-mal coordination variables and introducing a special transition link.The altitude of multi-vehicles are al-lowed to be changed in a certain range by using this proposed solution that considers the flight ability under the restraint of multi-vehicles formation mission and then realizes the accurate online control of the relative transverse and longitudinal range.Simulation results show that the proposed algorithm can achieve the de-sired control effect in scenarios of formation assembly and keeping,formation configuration switching and formation lateral maneuver.The algorithm takes into account the effects of the earth's curvature and rota-tion on the reentry dynamics,and can adapt to random aerodynamic coefficients and atmosphere density pulling by good robustness.

关键词

无动力飞行器/编队保持/构型切换/一致性跟踪控制

Key words

Unpowered vehicle/Formation keeping/Configuration switching/Consistency tracking con-trol

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出版年

2024
航天控制
北京航天自动控制研究所

航天控制

CSTPCDCSCD
影响因子:0.29
ISSN:1006-3242
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