Hurdle-Hop Simulation of Tilt-Rotor Aircraft Based on Optimal Control Theory
Aiming at simulating the hurdle-hop of tilt-rotor aircraft in forward flight near the ground, two models of numerical simulation and analysis based on optimal control theory were proposed. Firstly, Longitudinal flight dynamic model for tilt-rotor was modified considering the influence of ground effe...
| Format: | Article |
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| Language: | zho |
| Published: |
The Northwestern Polytechnical University
2020-12-01
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| Series: | Xibei Gongye Daxue Xuebao |
| Subjects: | |
| Online Access: | https://www.jnwpu.org/articles/jnwpu/full_html/2020/06/jnwpu2020386p1266/jnwpu2020386p1266.html |