Coupled Dynamics and Integrated Control for Position and Attitude Motions of Spacecraft: A Survey
Author:
Affiliation:
1. Research and Development Center, China Academy of Launch Vehicle Technology,Beijing,China,100076
2. Center for Control Science and Technology, Southern University of Science and Technology,Shenzhen,518055
Publisher
Institute of Electrical and Electronics Engineers (IEEE)
Subject
Artificial Intelligence,Information Systems,Control and Systems Engineering,Control and Optimization
Link
http://xplorestaging.ieee.org/ielx7/6570654/10302455/10302432.pdf?arnumber=10302432
Reference273 articles.
1. Integrated Adaptive Control for Spacecraft Attitude and Orbit Tracking Using Disturbance Observer
2. Adaptive sliding mode control for six-DOF relative motion of spacecraft with input constraint
3. Experimental Validation of Positive Adaptive-Control Approach for Spacecraft Proximity Maneuvers
4. Fast adaptive pose tracking control for satellites via dual quaternion upon non-certainty equivalence principle
5. Automated Transfer Vehicle - A European versatile multi-mission vehicle
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1. Modelling Rigid Body Potential of Small Celestial Bodies for Analyzing Orbit–Attitude Coupled Motions of Spacecraft;Aerospace;2024-05-05
2. Attitude Tracking Control of Launcher with Structural Misalignment Based on Fully-Actuated System Approach;2023 2nd Conference on Fully Actuated System Theory and Applications (CFASTA);2023-07-14
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