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Data-driven game-based control of microsatellites for attitude takeover of target spacecraft with disturbance.
Chai, Yuan; Luo, Jianjun; Ma, Weihua.
Afiliação
  • Chai Y; Research and Development Institute of Northwestern Polytechnical University in Shenzhen, Shenzhen, 518057, China; Science and Technology on Aerospace Flight Dynamics Laboratory, Northwestern Polytechnical University, Xi'an, 710072, China.
  • Luo J; Research and Development Institute of Northwestern Polytechnical University in Shenzhen, Shenzhen, 518057, China; Science and Technology on Aerospace Flight Dynamics Laboratory, Northwestern Polytechnical University, Xi'an, 710072, China. Electronic address: jjluo@nwpu.edu.cn.
  • Ma W; Research and Development Institute of Northwestern Polytechnical University in Shenzhen, Shenzhen, 518057, China; Science and Technology on Aerospace Flight Dynamics Laboratory, Northwestern Polytechnical University, Xi'an, 710072, China.
ISA Trans ; 119: 93-105, 2022 Jan.
Article em En | MEDLINE | ID: mdl-33676736
ABSTRACT
This paper investigates the problem of using multiple microsatellites to control the attitude of a target spacecraft losing control ability. Considering external disturbance and unknown system dynamics, a data-driven robust control method based on game theory is proposed. Firstly, the attitude takeover control of the target using multiple microsatellites is modeled as a robust differential game among disturbance and multiple microsatellites, in which microsatellites can obtain the worst-case control policies. Subsequently, policy iteration algorithm is put forward to acquire the robust Nash equilibrium control policies of microsatellites with known dynamics, which is a basis of data-driven algorithm. Then, by employing off-policy integral reinforcement learning, a data-driven online controller without information about system dynamics is developed to get the feedback gain matrices of microsatellites by learning robust Nash equilibrium solution from online input-state data. To validate the effectiveness of the proposed control method, numerical simulations are provided.
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Texto completo: 1 Base de dados: MEDLINE Idioma: En Ano de publicação: 2022 Tipo de documento: Article

Texto completo: 1 Base de dados: MEDLINE Idioma: En Ano de publicação: 2022 Tipo de documento: Article