Analysis on controllability and stability of quad-tilt-rotor aircraft in helicopter mode
The controllability and stability of quad-tilt-rotor aircraft in helicopter mode are modeled and analyzed, which will provide a theoretical guidance for the subsequent control system design. First of all, the flight dynamics model is established considering rotor-wing interference and verified with...
| Format: | Article |
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| Language: | zho |
| Published: |
The Northwestern Polytechnical University
2021-06-01
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| Series: | Xibei Gongye Daxue Xuebao |
| Subjects: | |
| Online Access: | https://www.jnwpu.org/articles/jnwpu/full_html/2021/03/jnwpu2021393p675/jnwpu2021393p675.html |