Design of integrated pitch axis for autopilot/autothrottle and integrated lateral axis for autopilot/yaw damper for NASA TSRV airplane using integral LQG methodology /
Isaac Kaminer ... [et al.].

APA Citation

Kaminer, I., Langley Research Center., Boeing Commercial Airplane Company. (1990). Design of integrated pitch axis for autopilot/autothrottle and integrated lateral axis for autopilot/yaw damper for NASA TSRV airplane using integral LQG methodology. Washington, D.C.: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division .

MLA Citation

Kaminer, Isaac, Langley Research Center, and Boeing Commercial Airplane Company. Design of Integrated Pitch Axis for Autopilot/autothrottle And Integrated Lateral Axis for Autopilot/yaw Damper for NASA TSRV Airplane Using Integral LQG Methodology. Washington, D.C.: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division , 1990.

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