Description and preliminary studies of a computer drawn instrument landing approach display
James J. Adams, Frederick J. Lallman, United States. National Aeronautics and Space Administration. Scientific and Technical Informtion Office, Langley Research Center
National Aeronautics and Space Administration, Scientific and Technical Information Office, 1978 - Technology & Engineering - 42 pages
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92 meters aircraft attitude aircraft reference symbol airplane coordinates alined APPENDIX approach path attitude indicator axis system BA BA Box at 92 box display box located cathode-ray tube continuous tracking corresponding pilot-model—aircraft system Cross pointer Box cross pointer display cross pointer instrument damping ratio defined desired path direction cosines displacement error draw the box equations heading angle histories of lateral inner-loop jB(sin landing approach displays Langley Research Center lateral and vertical lateral control Lateral step correction lateral-displacement error Line Vector Origin Longitudinal m/sec NASA needed to draw obtained with subject Pilot model Kn Pilot-Model Analysis pilot-model gains pilot-model—aircraft system match pointer and attitude Pointing distance pointing reference rad/m rad/sec range of 92 raw displacement data Root-mean-square sec Subject shown in figure step corrections obtained Subject G Subject K Pilot system response characteristics transformation matrix turbulence vertical step corrections Window Y-axis Window Z-axis