Wave-Based Attitude Control of Spacecraft with Fuel Sloshing Dynamics
نویسندگان
چکیده
منابع مشابه
Attitude stabilization of a rigid spacecraft using two control torques: A nonlinear control approach based on the spacecraft attitude dynamics
-The attitude stabilization problem of a rigid spacecraft using control torques supplied by gas jet actuators about only two of its principal axes is considered. If the uncontrolled principal axis of the spacecraft is not an axis of symmetry, then the complete spacecraft dynamics are small time locally controllable. However, the spacecraft cannot be asymptotically stabilized to any equilibrium ...
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ژورنال
عنوان ژورنال: Archive of Mechanical Engineering
سال: 2016
ISSN: 2300-1895
DOI: 10.1515/meceng-2016-0015