Conference proceeding
Online identification and control of linearized aircraft dynamics
Proceedings of the IEEE 1992 National Aerospace and Electronics Conference@m_NAECON 1992, v 2, pp 497-502
1992
Abstract
The authors examine a novel approach to online identification and control that requires substantially weaker excitation and works in closed-loop systems. This approach also uses multiple objective optimization theory to resolve the conflict between identification and controller performance as they compete for the only available resource, the inputs to the aircraft. The approach is applied to a longitudinal model of a representative linearized high-performance aircraft model. Simulation results compare the final controller with a conventional gain scheduled pitch command augmentation system. It is demonstrated that, by allowing some control input to be given to the identification process, the controller's overall performance is improved.< >
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Details
- Title
- Online identification and control of linearized aircraft dynamics
- Creators
- I Rusnak - Drexel UniversityM SteinbergA GuezI Bar-KanaIEEE
- Publication Details
- Proceedings of the IEEE 1992 National Aerospace and Electronics Conference@m_NAECON 1992, v 2, pp 497-502
- Conference
- IEEE 1992 National Aerospace and Electronics Conference NAECON 1992
- Publisher
- IEEE
- Number of pages
- 1
- Resource Type
- Conference proceeding
- Language
- English
- Academic Unit
- Electrical and Computer Engineering
- Web of Science ID
- WOS:A1992BW68D00071
- Other Identifier
- 991019182755904721
InCites Highlights
Data related to this publication, from InCites Benchmarking & Analytics tool:
- Web of Science research areas
- Engineering, Aerospace