刚体卫星相平面控制闭环系统稳定性分析

doi:10.3969/j.issn.1674-1579.2018.01.001

Abstract

Abstract: Abstract：Considering the problem of stability analysis of the satellite attitude system controlled by a phaseplane controller, a simplified phaseplane control method is proposed, and then the stability of the rigid satellite attitude system under the proposed controller is investigated in detail. By estimating the closedloop system’s trajectories with the phaseplane analysis method, the existence of a stable region of the closedloop system is proved, which satisfies certain properties. The formula to determine the stable region is derived in terms of control parameters. Under certain conditions, it is proved that the trajectories can reach the stable region in finite time from any initial value. Therefore, the sufficient condition is obtained to guarantee the globally uniformly ultimate boundedness of the closedloop system. In addition, the formula to estimate the reach time is provided. Simulations are provided to illustrate the effectiveness of proposed formulas and methods.

Key words: Keywords：rigid satellite, phaseplane control, stability, phaseplane analysis, reachability, globally uniformly ultimate boundedness

CLC Number:

V448.2

CHEN Zhi-Hua, XIE Yong-Chun. Stability Analysis of the ClosedLoop System of a PhasePlane Controlled Rigid Satellite[J]., 2018, 44(1): 1-14.

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URL: http://journal01.magtech.org.cn/Jwk3_kjkzjs/EN/10.3969/j.issn.1674-1579.2018.01.001

http://journal01.magtech.org.cn/Jwk3_kjkzjs/EN/Y2018/V44/I1/1

References

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Stability Analysis of the ClosedLoop System of a PhasePlane Controlled Rigid Satellite

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