Analysis of aircraft pitch axis stability augmentation system using sum of squares optimization

Analysis of aircraft pitch axis stability augmentation system using sum of squares optimization

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The aircraft pitch axis stability augmentation system was analyzed using sum of squares optimization. The nonlinear dynamics of the pitch axis of a fictitious Aircraft - the Robust Civil Aircraft Model (RCAM) was considered. A LTI dynamic inversion based control law for the short period dynamics of...

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Dades bibliogràfiques
Autors principals:	Krishnaswamy, K, Papageorgiou, G, Glavaski, S, Papachristodoulou, A
Format:	Journal article
Idioma:	English
Publicat:	2005

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