Smooth sliding-mode control for spacecraft attitude tracking maneuvers

Author:

Lo Shih-Che1,Chen Yon-Ping1

Affiliation:

1. National Chiao Tung University, Hsinchu 300, Taiwan, Republic 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

Cited by 195 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. Geometric tracking on 3 based on sliding mode control;International Journal of Robust and Nonlinear Control;2024-06-12

2. Robust Attitude Tracking Control Based on Adaptive Dynamic Programming for Flexible Dumbbell-Shaped Spacecraft;IEEE Transactions on Aerospace and Electronic Systems;2024-04

3. Simple robust PD control for asymptotic stabilization of uncertain spacecraft with actuator constraints and disturbances;International Journal of Robust and Nonlinear Control;2024-03-15

4. Velocity-Free Attitude Control with Actuator Constraint;Advanced Attitude Control of Satellite;2024

5. Overview;Advanced Attitude Control of Satellite;2024

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