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带时变通信时间延迟的卫星编队姿态协同自适应L2增益控制
引用本文:周稼康,胡庆雷,马广富,吕跃勇.带时变通信时间延迟的卫星编队姿态协同自适应L2增益控制[J].航空学报,2011,32(2):321-329.
作者姓名:周稼康  胡庆雷  马广富  吕跃勇
作者单位:哈尔滨工业大学航天学院,黑龙江哈尔滨,150001
基金项目:国家自然科学基金,高等学校博士学科点专项科研基金,黑龙江省留学回国人员科学基金,哈尔滨市留学回国基金,中央高校基本科研业务费专项基金
摘    要:针对卫星编队姿态协同分布式控制问题,提出一种基于Lyapunov方法的编队飞行协同控制策略.首先,考虑到实际编队飞行中星问通信存在时变时间延迟及模型不确定问题,结合变结构控制的思想设计一种针对时滞系统稳定性分析的Lyapunov函数,从而由直接Lyapunov方法得到可对模型参数进行估计的自适应分布式姿态协同控制器,并...

关 键 词:编队飞行  协同控制  L2增益扰动抑制  时间延迟  Lyapunov函数

Adaptive L2-gain Cooperative Attitude Control of Satellite Formation Flying with Time-varying Delay
ZHOU Jiakang,HU Qinglei,MA Guangfu,LU Yueyong.Adaptive L2-gain Cooperative Attitude Control of Satellite Formation Flying with Time-varying Delay[J].Acta Aeronautica et Astronautica Sinica,2011,32(2):321-329.
Authors:ZHOU Jiakang  HU Qinglei  MA Guangfu  LU Yueyong
Institution:ZHOU Jiakang,HU Qinglei,MA Guangfu,LU Yueyong School of Astronautics,Harbin Institute of Technology,Harbin 150001,China
Abstract:This article develops a new Lyapunov design based cooperative attitude control scheme for satellite formation flying with time-varying delay by explicitly taking attitude tracking performance into account. First, this article introduces a proper Lyapunov function to design an adaptive variable structure control law, with this control law the model uncertainties, external disturbances and even variable time-delay in the inter-satellite communication are explicitly considered simultaneously. Second, the tracking performance is evaluated by L2-gain from the disturbance input to the penalty output. The novelty of the approach lies in the strategy to construct such a Lyapunov function scarifying the L2-gain dissipative inequation that ensures not only the stability of a cooperative attitude tracking formation system but also an L2-gain constraint on the tracking performance. This provides a better closed-form solution to depress the external disturbances in order to achieve a better output performance for satellite formation flying cooperative attitude control as compared with the conventional methods. Complete stability and performance analysis is presented and illustrative simulation results of an application to satellite formation flying show that high precision attitude control with zero steady-error is successfully achieved using various scenarios of time-delay.
Keywords:formation flying  cooperative control  L  time delay  Lyapunov function
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