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

عرض إصدارات أخرى (2)

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...

وصف كامل

التفاصيل البيبلوغرافية
المؤلفون الرئيسيون:	Krishnaswamy, K, Papageorgiou, G, Glavaski, S, Papachristodoulou, A
التنسيق:	Journal article
اللغة:	English
منشور في:	2005

مواد مشابهة

Analysis of aircraft pitch axis stability augmentation system using sum of squares optimization
حسب: Krishnaswamy, K, وآخرون
منشور في: (2005)

Analysis of aircraft pitch axis stability augmentation system using sum of squares optimization
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منشور في: (2005)

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