Simulator evaluation of the effects of reduced spoiler and thrust authority on a decoupled longitudinal control system during landings in wind shear
By: G. Kimball Miller, Jr
Contributors: United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch; Langley Research Center
Series: NASA technical memorandum -- 83188
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Branch; For sale by the National Technical Information Service]
Published: 1981
Place of publication: Washington, D.C; [Springfield, Va
Language: eng
Number of pages: 48
Subjects: Stability of airplanes, Longitudinal; Airplanes -- Control systems; Vertical wind shear
Notes: "Langley Research Center."

"October 1981"--Cover

Subject Category 08

Inncludes bibliographical references