Design of Flight Control Law of Tilt-Rotor Aircraft Based on Incremental Nonlinear Dynamic Inversion
International conference on guidance, navigation and control
01.01.2022
14 pages
Aufsatz (Konferenz)
Englisch
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Design of Flight Control Law of Tilt-Rotor Aircraft Based on Incremental Nonlinear Dynamic Inversion
Springer Verlag | 2021
|Incremental Nonlinear Dynamic Inversion and Control Allocation for a Tilt Rotor UAV (AIAA 2014-0963)
British Library Conference Proceedings | 2014
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