Inertia-Free Spacecraft Attitude Control Using Reaction Wheels
نویسندگان
چکیده
منابع مشابه
Inertia-Free Spacecraft Attitude Control Using Reaction Wheels
This paper extends the continuous inertia-free control law for spacecraft attitude tracking derived in prior work to the case of three axisymmetric reaction wheels. The wheels are assumed to be mounted in a known and linearly independent, but not necessarily orthogonal, configuration with an arbitrary and unknown orientation relative to the unknown spacecraft principal axes. Simulation results ...
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ژورنال
عنوان ژورنال: Journal of Guidance, Control, and Dynamics
سال: 2013
ISSN: 0731-5090,1533-3884
DOI: 10.2514/1.58363