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Integrated Flight/Propulsion Control Design Techniques Starting with the Engine
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English
Abstract
New techniques are being developed to determine the analytical design and hardware implementation of multivariable control systems for complex aircraft propulsion systems. The analytical design can be accomplished with applied optimal control theory. Hardware configuration trade studies can be used to determine the best way to implement the propulsion system for a particular aircraft. These techniques may be expanded to the design of integrated flight/propulsion control systems.
Authors
Citation
Sevich, G. and Beattie, E., "Integrated Flight/Propulsion Control Design Techniques Starting with the Engine," SAE Technical Paper 740481, 1974, https://doi.org/10.4271/740481.Also In
References
- Michael Gerald J. Farrar Florence A. “Development of Optimal Control Modes for Advanced Technology Propulsion Systems.” Interim Technical Report-Contract N00014-73-C-0281 August 1973 UARL Report M911620-1
- Lasdon L. S. Mitter S. K. Waren A. D. “The Conjugate Gradient Method for Optimal Control Problems.” IEEE Transactions on Automatic Control AC-12 2 April 1967 132 138
- Lasdon L. S. Waren A. D. “Mathematical Programming for Optimal Design.” Electro-Technology November 1967 53 70
- Navy Contract N00019-72-C-0612, Advanced Propulsion System for V/STOL Aircraft