Design of Flight Control Law of Tilt-Rotor Aircraft Based on Incremental Nonlinear Dynamic Inversion
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Publisher
Springer Singapore
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https://link.springer.com/content/pdf/10.1007/978-981-15-8155-7_391
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1. Multirotor VTOL and Tilt Rotor Transition to Fixed Wing;2023 IEEE 11th International Conference on Systems and Control (ICSC);2023-12-18
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