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...
Main Authors: | Krishnaswamy, K, Papageorgiou, G, Glavaski, S, Papachristodoulou, A |
---|---|
פורמט: | Journal article |
שפה: | English |
יצא לאור: |
2005
|
פריטים דומים
-
Analysis of aircraft pitch axis stability augmentation system using sum of squares optimization
מאת: Krishnaswamy, K, et al.
יצא לאור: (2005) -
Analysis of aircraft pitch axis stability augmentation system using sum of squares optimization
מאת: Krishnaswamy, K, et al.
יצא לאור: (2005) -
Robust stability and performance analysis of a longitudinal aircraft model using sum of squares techniques
מאת: Papachristodoulou, A, et al.
יצא לאור: (2005) -
Generalised absolute stability and sum of squares.
מאת: Hancock, E, et al.
יצא לאור: (2013) -
Generalised absolute stability and sum of squares
מאת: Hancock, E, et al.
יצא לאור: (2013)