Aggressive flight control of quadrotors using incremental nonlinear dynamic inversion with a high-fidelity thrust unit model
DOI10.1016/J.JFRANKLIN.2024.106914zbMATH Open1541.93242MaRDI QIDQ6559355
Xiaojie Su, Zeliang Wu, Tao Song, Jianchuan Ye, Tao Jiang
Publication date: 21 June 2024
Published in: Journal of the Franklin Institute (Search for Journal in Brave)
incremental nonlinear dynamic inversionaggressive flight controlflight maneuverabilityhigh-fidelity thrust modelpole distribution-based analysis
Nonlinear systems in control theory (93C10) Automated systems (robots, etc.) in control theory (93C85)
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