A Total Energy Attitude Control System Strategy for Rigid Spacecraft
This paper aims to design a controller based on the Total Energy Control System (TECS) method, to solve the attitude trajectory tracking problem for rigid spacecraft. TECS objective is to command the total energy rate using a proportional-integral (PI) controller. The attitude control objective fixe...
| Main Authors: | , |
|---|---|
| Format: | Article |
| Language: | English |
| Published: |
IEEE
2019-01-01
|
| Series: | IEEE Access |
| Subjects: | |
| Online Access: | https://ieeexplore.ieee.org/document/8794491/ |