一种控制系统故障处理中的互斥设计方法

doi:10.3969/j.issn.1674-1579.2021.01.012

Abstract

Abstract: The thruster need to be switched if some kind of fault in spacecraft control system occurs. Spacecraft thruster switching takes multiple software control cycles to complete, so it can’t be interrupted during execution. The sequence conflict and failure of thruster switching due to crosscoupled occurrence of multiple fault disposals are fully analyzed. A software mutually exclusive design method is presented in this paper for thruster switch failure. Simulation results show that this method is feasible.

Key words: control system, thruster switching, fault disposal, crosscoupling, mutually exclusive design

CLC Number:

V249

WANG Qun, WU Peiya, CHEN Zhihua, ZHOU Zhongze, LI Guangxu. Mutually Exclusive Design of Control System and Fault Disposal[J].Aerospace Contrd and Application, 2021, 47(1): 87-92.

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URL: http://journal01.magtech.org.cn/Jwk3_kjkzjs/EN/10.3969/j.issn.1674-1579.2021.01.012

http://journal01.magtech.org.cn/Jwk3_kjkzjs/EN/Y2021/V47/I1/87

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Mutually Exclusive Design of Control System and Fault Disposal

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