Anti-Disturbance Backstepping Attitude Control for Rigid-Flexible Coupling Spacecraft
This paper investigates the problem of attitude stabilization for rigid-flexible coupling spacecraft under external disturbances, parametric uncertainties, and measurement errors. First, the dynamical model for a rigid spacecraft with two symmetric solar arrays is derived based on the Lagrange metho...
| Main Authors: | , , |
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| Format: | Article |
| Language: | English |
| Published: |
IEEE
2018-01-01
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| Series: | IEEE Access |
| Subjects: | |
| Online Access: | https://ieeexplore.ieee.org/document/8454358/ |