Design of integrated pitch axis for autopilot/autothrottle and integrated lateral axis for autopilot/yaw damper for NASA TSRV airplane using integral LQG methodology
By: Isaac Kaminer ... [et al.].
Contributors: Kaminer, Isaac.; United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.
Series: NASA contractor report -- 4268.; NASA contractor report -- NASA CR-4268.
Publisher: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division
Published: 1990
Place of publication: [Washington, DC]
Language: eng
Format: Microform
Subjects: Stability of airplanes, Longitudinal.; Stability of airplanes, Lateral.; Automatic pilot (Airplanes)
Notes: Distributed to depository libraries in microfiche.

Microfiche. [Washington, D.C.? : National Aeronautics and Space Administration], 1990. 2 microfiches.