PD control and the unwinding effect in quaternion parameterized attitude control
Author:
Affiliation:
1. Budapest University of Technology and Economics,Department of Control Engineering and Information Technology,Budapest,Hungary
Publisher
IEEE
Link
http://xplorestaging.ieee.org/ielx7/10297583/10297621/10297790.pdf?arnumber=10297790
Reference20 articles.
1. Fixed-time regulation of spacecraft orbit and attitude coordination with optimal actuation allocation using dual quaternion
2. Adaptive finite-time control for six-degree-of-freedom leader-following spacecraft formation using twistors
3. Spacecraft relative rotation tracking without angular velocity measurements
4. Globally asymptotically stable ‘PD+’ controller for robot manipulators
5. Anti-unwinding terminal sliding mode attitude tracking control for rigid spacecraft
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1. Simultaneous attitude and position tracking using dual quaternion parameterized dynamics;2024 IEEE 22nd World Symposium on Applied Machine Intelligence and Informatics (SAMI);2024-01-25
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