Helicopter Landing Trajectory Optimization after Tail Rotor Control Failure in Different Collective Pitch
This paper studies helicopter optimal landing and control procedure after tail rotor control failure (TRCF) in different collective pitch. The optimal control problem of landing after tail rotor control failure was solved numerically by direct multiple shooting method and sequential quadratic progra...
| Format: | Article |
|---|---|
| Language: | zho |
| Published: |
EDP Sciences
2019-12-01
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| Series: | Xibei Gongye Daxue Xuebao |
| Subjects: | |
| Online Access: | https://www.jnwpu.org/articles/jnwpu/full_html/2019/06/jnwpu2019376p1138/jnwpu2019376p1138.html |