Three-dimensional, minimum fuel turns for a supersonic aircraft-Reference-Cited by-同舟云学术

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Three-dimensional, minimum fuel turns for a supersonic aircraft

Published:1971-08-16 Issue: Volume: Page:
ISSN:
Container-title:Guidance, Control and Flight Mechanics Conference
language:
Short-container-title:

Author:

BRYSON, JR. A.¹

Affiliation:

1. STANFORD U., STANFORD, CALIF.

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1971-913

Reference22 articles.

1. In this paper altitude, bank angle and thrust pograms are determined which minimize the fuel required to turn through a specified heading angle and reach a specified energy. 71-913 vertical- mg

2. the 13,E Space 71-919 Minimum Fuel, Increasing Energy Turns With Final Heading Angle Specified

Cited by 2 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Aircraft Maneuver Optimization by Reduced-Order Approximation* *The research was performed in part under Contract NAS 12-656 with NASA Electronics Research Center and Contract F 44620-71-C-0123 with USAF Headquarters, Office of the Assistant Chief of Staff for Studies and Analysis.;Control and Dynamic Systems;1973

2. Three-Dimensional^ Minimum-Time Turns for a Supersonic Aircraft;Journal of Aircraft;1972-02

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