Momentum unloading excessive reaction-wheel system of a spacecraft
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Publication:734021
DOI10.1134/S1064230708040138zbMath1178.93104MaRDI QIDQ734021
Publication date: 19 October 2009
Published in: Journal of Computer and Systems Sciences International (Search for Journal in Brave)
asymptotic stabilitycontrol systems of spacecraftlinear algebraic equations as additional control parameters
Application models in control theory (93C95) Variable mass, rockets (70P05) Asymptotic stability in control theory (93D20) Control/observation systems governed by ordinary differential equations (93C15)
Related Items (2)
Unloading angular momentum for inertial actuators of a spacecraft in the pitch channel ⋮ Schemes of momentum/reaction wheels unloading by mechanical restructuring and gearbox for spacecraft
Cites Work
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