Finite-time attitude tracking control design for reusable launch vehicle in reentry phase based on disturbance observer
For the attitude tracking control problem of reentry reusable launch vehicle in reentry phase, a disturbance observer–based sliding mode controller is proposed in this article. At first, attitude model is decomposed into two loops on the basis of the engineering backgrounds of reusable launch vehicl...
| Main Authors: | , , , |
|---|---|
| Format: | Article |
| Language: | English |
| Published: |
SAGE Publishing
2017-12-01
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| Series: | Advances in Mechanical Engineering |
| Online Access: | https://doi.org/10.1177/1687814017744077 |