Abstract
This paper addresses the problem of spacecraft attitude and position synchronization in libration point orbits between a leader and a follower. Using dual quaternion, the dimensionless relative coupled dynamical model is derived considering computation efficiency and accuracy. Then a model-independent dimensionless cascade pose-feedback active disturbance rejection controller is designed to spacecraft attitude and position tracking control problems considering parameter uncertainties and external disturbances. Numerical simulations for the final approach phase in spacecraft rendezvous and docking and formation flying are done, and the results show high-precision tracking errors and satisfactory convergent rates under bounded control torque and force which validate the proposed approach.
Original language | English |
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Pages (from-to) | 238-249 |
Number of pages | 12 |
Journal | Acta Astronautica |
Volume | 145 |
DOIs | |
State | Published - Apr 2018 |
Keywords
- Active disturbance rejection controller
- Attitude and position synchronization
- Dual quaternion
- Libration point orbits