Design of integrated pitch axis for autopilot/autothrottle and integrated lateral axis for autopilot/yaw damper for NASA TSRV airplane using integral LQG methodology, Volume 4268

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National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990 - Technology & Engineering - 144 pages
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Contents

Longitudinal Axis Results
79
Lateral Axis Results
103
REFERENCES
144

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