应用分力合成主动振动抑制方法的最优飞行器大角度机动控制策略

ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 2002, Vol. 23 ›› Issue (1): 62-65.

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OPTIMAL LARGE ANGLE MANEUVER CONTROL STRATEGY OF SPACECRAFT WITH COMPONENT SYNTHESIS ACTIVE VIBRATION SUPPRESSION METHOD

SHAN Jin-jun, LIU Dun

Department of Astronautics and Mechanics, Harbin Institute of Technology, Harbin 150001, China

Received:2001-01-15 Revised:2001-07-26 Online:2002-02-25 Published:2002-02-25

Abstract

Abstract:

This paper puts forward a component synthesis active vibration suppression (CSVS) method for spacecraft with the large flexible appendage and analyzes its robustness to uncertainty in modeling parameters. This method can eliminate unwanted flexible vibration modes while achieves desired rigid motion; the robustness makes it practical in engineering. For a kind of spacecraft with constant amplitude reaction jet actuators, time-fuel optimal maneuver control strategies are designed using CSVS method. Simulation results validate this method.

Key words: component synthesis active vibration suppression method, optimal control, robustness, large anglemaneuver

SHAN Jin-jun;LIU Dun. OPTIMAL LARGE ANGLE MANEUVER CONTROL STRATEGY OF SPACECRAFT WITH COMPONENT SYNTHESIS ACTIVE VIBRATION SUPPRESSION METHOD[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2002, 23(1): 62-65.

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OPTIMAL LARGE ANGLE MANEUVER CONTROL STRATEGY OF SPACECRAFT WITH COMPONENT SYNTHESIS ACTIVE VIBRATION SUPPRESSION METHOD

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