Robust control of spacecraft rendezvous on elliptical orbit

Author:

Gao Xiangyu,Teo Kok Lay,Duan Guang-Ren

Publisher

Elsevier BV

Subject

Applied Mathematics,Computer Networks and Communications,Signal Processing,Control and Systems Engineering

Reference26 articles.

1. Terminal guidance system for satellite rendezvous;Clohessy;Journal of the Astronautical Sciences,1960

2. State transition matrices for terminal rendezvous studies;Carter;Journal of Guidance, Control and Dynamics,1998

3. Lyapunov differential equation approach to elliptical orbital rendezvous with constrained controls;Zhou;Journal of Guidance, Control and Dynamics,2011

4. Optimal sliding-mode guidance with terminal velocity constraint for fixed-interval propulsive maneuvers;Ebrahimi;Acta Astronautica,2008

5. Multi-objective robust H∞ control of spacecraft rendezvous;Gao;IEEE Transactions on Control Systems Technology,2009

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2. Adaptive Control of the Relative Position for Space Vehicles in the Rendezvous Missions;2023 27th International Conference on System Theory, Control and Computing (ICSTCC);2023-10-11

3. Robust Optimal Control of Spacecraft during the Rendezvous Missions using H Control Method;2023 27th International Conference on System Theory, Control and Computing (ICSTCC);2023-10-11

4. Spacecraft Attitude Control with Fully Actuated System and Particle Swarm Optimization Approaches;2023 2nd Conference on Fully Actuated System Theory and Applications (CFASTA);2023-07-14

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