Prescribed-time attitude control during solid thrusting orbital maneuver
Author:
Affiliation:
1. Northwestern Polytechnical University,School of Astronautics,Xi’an,China
Funder
National Natural Science Foundation of China
Publisher
IEEE
Link
http://xplorestaging.ieee.org/ielx7/10005874/10005887/10006308.pdf?arnumber=10006308
Reference23 articles.
1. Finite time control strategy for satellite attitude maneuver based on hybrid actuator
2. Retrofiring control method via combination of a 1DoF gimbaled thrust vector control and spin-stabilization
3. Attitude stabilization of rigid spacecraft with finite-time convergence
4. Robust finite-time adaptive control algorithm for satellite fast attitude maneuver
5. Finite‐time attitude‐tracking control for rigid spacecraft with actuator failures and saturation constraints
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