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Integrated Flight/Propulsion Control for Next Generation Military Aircraft

SAE Technical Papers (1906-current) Available online

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Format:
Conference/Event
Author/Creator:
SMALL, LESTER L., author.
Conference Name:
SAE Aerospace Technology Conference and Exposition (1986-10-13 : Long Beach, California, United States)
Language:
English
Physical Description:
1 online resource
Place of Publication:
Warrendale, PA SAE International 1986
Summary:
The integration of flight and propulsion control systems on future military aircraft offers the potential for improved steady state and dynamic performance while tolerating faults generated by component failures and battle damage. Achieving this capability will require improved modeling, advances in control and fault-accommodation logic, and redundant computer system architectures with appropriate communication capabilities. Integration of associated systems, such as hydraulic and electrical power, fuel distribution and thermal management, and environmental control, will also be required. Finally, a new management perspective will be needed in both industry and government sectors to foster and mature these "technologies of integration"
Notes:
Vendor supplied data
Publisher Number:
861726
Access Restriction:
Restricted for use by site license

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