Krishnaswamy, Kailash and Papageorgiou, George and Glavaski, Sonja and Papachristodoulou, Antonis (2005) Analysis of aircraft pitch axis stability augmentation system using sum of squares optimization. In: Proceedings of the 2005 American Control Conference. Proceedings of the American Control Conference. IEEE , Piscataway, NJ, pp. 2701-2702. ISBN 0-7803-9098-9 http://resolver.caltech.edu/CaltechAUTHORS:20110609-133753780
- Published Version
See Usage Policy.
Use this Persistent URL to link to this item: http://resolver.caltech.edu/CaltechAUTHORS:20110609-133753780
The region of attraction of a trim point for the pitch axis of a nonlinear modeled aircraft modulated via linear dynamic inversion based controller was determined numerically. The model incorporates uncertainty in the position of center of gravity along the X-body axis. The stability regions are computed using SOSTOOLS, which converts the required sum of squares conditions to an appropriate semi definite program that is then solved using SeDuMi.
|Item Type:||Book Section|
|Additional Information:||© 2005 AACC. Issue Date: 8-10 June 2005. Date of Current Version: 01 August 2005.|
|Other Numbering System:|
|Official Citation:||Krishnaswamy, K.; Papageorgiou, G.; Glavaski, S.; Papachristodoulou, A.; , "Analysis of aircraft pitch axis stability augmentation system using sum of squares optimization," American Control Conference, 2005. Proceedings of the 2005 , vol., no., pp. 2701- 2702 vol. 4, 8-10 June 2005 doi: 10.1109/ACC.2005.1470375 URL: http://ieeexplore.ieee.org/stamp/stamp.jsp?tp=&arnumber=1470375&isnumber=31519|
|Usage Policy:||No commercial reproduction, distribution, display or performance rights in this work are provided.|
|Deposited By:||Tony Diaz|
|Deposited On:||14 Jun 2011 18:50|
|Last Modified:||23 Aug 2016 00:02|
Repository Staff Only: item control page