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.].
Description
- Language(s)
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English
- Published
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Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; 1990.
- Note
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Prepared at Boeing Commercial Airplane Company for Langley Research Center under Contract NAS1-18027.
- Physical Description
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vii, 144 p. :
ill. ;
28 cm.
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University of Illinois at Urbana-Champaign
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