Design of Flight Control Law of Tilt-Rotor Aircraft Based on Incremental Nonlinear Dynamic Inversion
International Conference on Guidance, Navigation and Control ; 2020 ; Tientsin
2022
Conference paper
English
Design of Flight Control Law of Tilt-Rotor Aircraft Based on Incremental Nonlinear Dynamic Inversion
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|FULL-LENGTH PAPERS - Adaptive Model Inversion Flight Control for Tilt-Rotor Aircraft
Online Contents | 1999
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