一种偏置动量卫星的三轴姿态控制方法

Abstract

Abstract: A 2-Degree-of-Freedom(DOF)control wheel configuration in the roll/yaw plane is presented for the satellite attitude control．On the basis of analysis of environmental disturbance torques to some communications satellite platform，the wheel configuration is compared with the existing four-wheel pyramidal configuration according to parameters such as effect of biased momentum magnitude，storage capability，maximum momentum variation，reliability．It is concluded that the proposed configuration exceeds the four-wheel pyramidal configuration in performances．

Key words: font-family:Calibri, sans-serif, momentum-bias control">momentum-bias controlfont-family:宋体, ')">">, font-family:Calibri, sans-serif, communications satellite">communications satellitefont-family:宋体, ')">">, font-family:Calibri, sans-serif, attitude control">attitude controlfont-family:宋体, ')">">, font-family:Calibri, sans-serif, wheel configuration">wheel configuration')">">

CLC Number:

WU Dan. A Method for Three Axis Attitude Control of Momentum Bias Satellite[J].Aerospace Contrd and Application, 2008, 34(3): 51-54.

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/ / Recommend momentum-bias control；communications satellite；attitude control；wheel configuration”. Please open it by linking:http://journal01.magtech.org.cn/Jwk3_kjkzjs/EN/abstract/abstract9409.shtml" name="neirong"> momentum-bias control；communications satellite；attitude control；wheel configuration">

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A Method for Three Axis Attitude Control of Momentum Bias Satellite

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