Bifurcation analysis for a novel flight vehicle with pitch-control single moving mass

Moving mass flight vehicle is a strongly nonlinear system under high speed flying conditions. The system attitude dynamics becomes even more complex due to the coupling between the internal moving mass with large mass ratio and the vehicle body. This article investigates the open-loop nonlinear dyna...

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Veröffentlicht in:	Proceedings of the Institution of Mechanical Engineers. Part G, Journal of aerospace engineering Journal of aerospace engineering, 2022-03, Vol.236 (4), p.802-810
Hauptverfasser:	Liu, Zhitao, Li, Jianqing, Gao, Changsheng, Jing, Wuxing
Format:	Artikel
Sprache:	eng
Schlagworte:	Bifurcation theory Continuation methods Dynamical systems Flight vehicles Nonlinear dynamics Nonlinear systems Parameters Pitch (inclination) Static stability
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