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The Integration of Adaptive Cooperative Control for Position...

The Integration of Adaptive Cooperative Control for Position and Attitude of Distributed Spacecraft

作     者:Yaen Xie Zhen Shi Chuqi Sun Yue Deng Xiande Wu 

作者单位:College of AutomationHarbin Engineering University College of Aerospace and Civil EngineeringHarbin Engineering University 

会议名称:《第36届中国控制会议》

会议届次:36

主办单位:Dalian University of Technology;Systems Engineering Society of China (SESC);Technical Committee on Control Theory (TCCT), Chinese Association of Automation (CAA)

会议日期:2017年

学科分类:08[工学] 081105[工学-导航、制导与控制] 0811[工学-控制科学与工程] 

基  金:partially funded by the National High Technology Research and Development Program of China(no.2013AA122904) the Fundamental Research Funds for the Central Universities(no.HEUCFD1503) the Natural Science Foundation of Heilongjiang Province(no.F2015032) the National Natural Science Funds(no.11302127) the Harbin Science and Technology Innovation Talent Youth Fund(no.2013RFQXJ001) Postdoctoral Science-Research Foundation(no.LBH-Q13042) 

关 键 词:Distributed Spacecraft Adaptive Cooperative Control Dual Quaternion Position and Attitude Integration 

摘      要:It is an important guarantee to ensure highly reliability,strong adaptability of distributed spacecraft that the adaptive cooperatives control for integration of the attitude and *** to the performance requirement of the distributed spacecraft in the process of configuration adjustment,there is established a integration model of position and attitude based on dual quaternion,and design a cooperative controller based on sliding mode variable structure *** on which we derive the adaptive cooperative control algorithm for distributed spacecraft integration of position and attitude by introducing the interference estimating algorithm through extended least squares method and weight algorithm of multi-spacecraft’s ***,mathematical simulation has been done to verify the stability and efficiency of the designed *** adaptive cooperative control algorithm for distributed spacecraft covers integration of position and attitude,collaboration requirement of multi-spacecraft and environment interference,and also ensures the performance for its efficiency,stability,and cooperation,which enhances system’s control ability.

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