The Principal Fiber Bundle Structure of the Gimbal-Spacecraft System
نویسندگان
چکیده
Nomenclature β,γ(∈ S) = The gimbal and wheel angles. (rad) Rβ(∈ SO(3)) = Transformation from gimbal frame G to the spacecraft body frame B. Is = Spacecraft inertia without the CMG gimbal and wheel inertia. (kg.m) Ig, Ir = Gimbal frame inertia, wheel inertia about own centre of mass represented in gimbal frame. (kg.m) (Igr)β = Combined inertia of gimbal frame and wheel in the spacecraft frame. RβIgrR β . (kg.m) Ĩ(β) = Locked inertia tensor.
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ورودعنوان ژورنال:
- CoRR
دوره abs/1706.07170 شماره
صفحات -
تاریخ انتشار 2017