Planned Fully Actuated Attitude Control Strategy for Flexible Spacecraft
Author:
Affiliation:
1. Nanjing University of Aeronautics and Astronautics,College of Astronautics,Nanjing,210006
Publisher
IEEE
Link
http://xplorestaging.ieee.org/ielx8/10595059/10595098/10595383.pdf?arnumber=10595383
Reference7 articles.
1. Disturbance observer-based constrained attitude control for flexible spacecraft
2. High-order fully actuated system approaches: Part I. Models and basic procedure
3. High-order fully-actuated system approaches: Part IX. Generalised PID control and model reference tracking
4. High-order fully-actuated system approaches: Part VI. Disturbance attenuation and decoupling
5. High-order fully actuated system approaches: Part VIII. Optimal control with application in spacecraft attitude stabilisation
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