Integrated Control of Position, Attitude, and Flexible Motion for Satellite Proximity Operations
Author:
Affiliation:
1. Mississippi State University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2009-5670
Reference33 articles.
1. Result of Autonomous Rendezvous Docking Experiment of Engineering Test Satellite-VII
2. 2Braukus,M.andNewton,K."OnOrbitAnomalyEndsDARTMissionEarly," http://www.nasa.gov/mission_pages/dart/media/05-051.html,2005.
3. Sliding mode control using modified Rodrigues parameters
4. Variable-structure control of spacecraft attitude maneuvers
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1. Coupled Dynamics and Integrated Control for Position and Attitude Motions of Spacecraft: A Survey;IEEE/CAA Journal of Automatica Sinica;2023-12
2. Integrated Translational and Rotational Control for the Final Approach Phase of Rendezvous and Docking;Asian Journal of Control;2018-03-08
3. Integrated relative position and attitude control of spacecraft in proximity operation missions;International Journal of Automation and Computing;2012-08
4. Optimal Attitude Control of Flexible Spacecraft with Minimum Vibration;AIAA Guidance, Navigation, and Control Conference;2010-06-26
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