Simulator evaluation of the effects of reduced spoiler and thrust authority on a decoupled longitudinal control system during landings in wind shear

  • 48 Pages
  • 1.43 MB
  • 6760 Downloads
  • English
by
National Aeronautics and Space Administration, Scientific and Technical Information Branch, For sale by the National Technical Information Service] , Washington, D.C, [Springfield, Va
Stability of airplanes, Longitudinal, Airplanes -- Control systems, Vertical wind
StatementG. Kimball Miller, Jr
SeriesNASA technical memorandum -- 83188
ContributionsUnited States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, Langley Research Center
The Physical Object
Pagination48 p. :
ID Numbers
Open LibraryOL14925817M