Dynamic Control Allocation for Shaping Spacecraft Attitude Control Command
نویسندگان
چکیده
منابع مشابه
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The stability of spacecraft attitude is studied with considering sinusoidal disturbance. A passive attitude controller without angular velocity measurement for spacecraft described by quaternion is designed. The passive controller has no information related to system parameters. So it has robustness to model error and uncertainty of model parameters. The stability of spacecraft attitude control...
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ژورنال
عنوان ژورنال: International Journal of Aeronautical and Space Sciences
سال: 2007
ISSN: 2093-274X
DOI: 10.5139/ijass.2007.8.1.010