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Optimal Turning Climb-Out and Descent of Commercial Jet Aircraft NASA Ames Research Center Moffett Field, CA

SAE Technical Papers (1906-current) Available online

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Format:
Conference/Event
Author/Creator:
Neuman, F., author.
Conference Name:
Aerospace Congress & Exposition (1982-10-25 : Anaheim, California, United States)
Language:
English
Physical Description:
1 online resource
Place of Publication:
Warrendale, PA SAE International 1982
Summary:
Optimal turning climb-out and descent flight-paths from and to runway headings are derived to provide the missing elements of a complete flight-path optimization for minimum fuel consumption. The paths are derived by generating a field of extremals, using the necessary conditions of optimal control. Results show that the speed profiles for straight and turning flight are essentially identical, except for the final horizontal accelerating or decelerating turn. The optimal turns, which require no abrupt maneuvers, could easily be integrated with present climb-cruise-descent fuel-optimization algorithms
Notes:
Vendor supplied data
Publisher Number:
821468
Access Restriction:
Restricted for use by site license

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