Integrated Flight/Propulsion Control Design Techniques Starting with the Engine 740481
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.
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. Download Citation
Author(s):
G. J. Sevich, E. C. Beattie
Affiliated:
Pratt & Whitney Aircraft Div., United Aircraft Corp.
Pages: 13
Event:
National Air Transportation Meeting
ISSN:
0148-7191
e-ISSN:
2688-3627
Also in:
SAE 1974 Transactions-V83-A
Related Topics:
Optimization
Control systems
Hardware
Aircraft
Starters and starting
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