Coupled Relative Orbit and Attitude Control Augmented by the Geomagnetic Lorentz Propulsions
Author:
Affiliation:
1. Tsinghua University, 100084 Beijing, People’s Republic of China
2. China Academy of Space Technology, 100094 Beijing, People’s Republic of China
3. Space Engineering University, 101416 Beijing, People’s Republic of China
Funder
China Postdoctoral Science Foundation
Natural Science Foundation of Hunan Province
National Natural Science Foundation of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering
Reference26 articles.
1. Linear Coupled Attitude–Orbit Control Through Aerodynamic Drag
2. New Synchronous Orbits Using the Geomagnetic Lorentz Force
3. Geometric Approach to Spacecraft Attitude Control Using Magnetic and Mechanical Actuation
4. Output Regulation Control for Satellite Formation Flying Using Differential Drag
5. Propellantless Stationkeeping at Enceladus via the Electromagnetic Lorentz Force
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