Optimal control of a programmed motion of a rigid spacecraft using redundant kinematics parameterizations
Author:
Publisher
Elsevier BV
Subject
General Mathematics,General Physics and Astronomy,Statistical and Nonlinear Physics,Applied Mathematics
Cited by 6 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. Optimal control of satellite attitude and its stability based on quaternion parameters;COMPUT METHODS DIFFE;2022
2. Robust optimal sliding mode control for spacecraft position and attitude maneuvers;Aerospace Science and Technology;2015-06
3. Finite-Time Anti-Disturbance Inverse Optimal Attitude Tracking Control of Flexible Spacecraft;Mathematical Problems in Engineering;2013
4. Optimal Output Feedback Controllers for Spacecraft Attitude Tracking;Asian Journal of Control;2012-09-27
5. Optimal Sliding Mode Controllers for Attitude Stabilization of Flexible Spacecraft;Mathematical Problems in Engineering;2011
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