Analysis of aircraft pitch axis stability augmentation system using sum of squares optimization
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...
Egile Nagusiak: | Krishnaswamy, K, Papageorgiou, G, Glavaski, S, Papachristodoulou, A |
---|---|
Formatua: | Journal article |
Hizkuntza: | English |
Argitaratua: |
2005
|
Antzeko izenburuak
-
Analysis of aircraft pitch axis stability augmentation system using sum of squares optimization
nork: Krishnaswamy, K, et al.
Argitaratua: (2005) -
Analysis of aircraft pitch axis stability augmentation system using sum of squares optimization
nork: Krishnaswamy, K, et al.
Argitaratua: (2005) -
Robust stability and performance analysis of a longitudinal aircraft model using sum of squares techniques
nork: Papachristodoulou, A, et al.
Argitaratua: (2005) -
Generalised absolute stability and sum of squares.
nork: Hancock, E, et al.
Argitaratua: (2013) -
Generalised absolute stability and sum of squares
nork: Hancock, E, et al.
Argitaratua: (2013)