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Development of high-angle-of-attack nose-down pitch control margin design guidelines for combat aircraft (1993)

Foster, John V. ; Ogburn, Marilyn E.

In: CASI

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Publication Date: 2013-08-31

Description: A broad research program to identify maneuvering requirements for advanced fighters and the corresponding design criteria to aid in making critical design tradeoffs is being conducted under the NASA High-Angle-of-Attack Technology Program (HATP). As part of this activity, NASA and the U.S. Navy are conducting cooperative research to develop high-angle-of-attack control margin requirements. This paper will summarize the status of this program. Following some background information, the simulation study conducted to develop a set of preliminary guidelines for nose-down pitch control is reviewed, and the results of some very limited flight tests are described.

Keywords: AIRCRAFT STABILITY AND CONTROL

Type: NASA LaRC Workshop on Guidance, Navigation, Controls, and Dynamics for Atmospheric Flight, 1993; p 293-322

Format: application/pdf

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