Attitude Blended Control for Aerospace Vehicle with Lateral Thrusters and Aerodynamic Fins
A finite-time blended control strategy is proposed for the reentry phase attitude control of the aerospace vehicle (ASV) based on the neural network, sliding mode control theory and control allocation. Firstly, a finite-time neural networks sliding mode controller is designed based on the attitude m...
| Format: | Article |
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| Language: | zho |
| Published: |
EDP Sciences
2019-06-01
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| Series: | Xibei Gongye Daxue Xuebao |
| Subjects: | |
| Online Access: | https://www.jnwpu.org/articles/jnwpu/full_html/2019/03/jnwpu2019373p532/jnwpu2019373p532.html |