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. https://resolver.caltech.edu/CaltechAUTHORS:20110609-133753780
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Abstract
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 | |||||||||
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| Additional Information: | © 2005 AACC. Issue Date: 8-10 June 2005. Date of Current Version: 01 August 2005. | |||||||||
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| Series Name: | Proceedings of the American Control Conference | |||||||||
| DOI: | 10.1109/ACC.2005.1470375 | |||||||||
| Record Number: | CaltechAUTHORS:20110609-133753780 | |||||||||
| Persistent URL: | https://resolver.caltech.edu/CaltechAUTHORS:20110609-133753780 | |||||||||
| 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. | |||||||||
| ID Code: | 23963 | |||||||||
| Collection: | CaltechAUTHORS | |||||||||
| Deposited By: | Tony Diaz | |||||||||
| Deposited On: | 14 Jun 2011 18:50 | |||||||||
| Last Modified: | 09 Nov 2021 16:19 |
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