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

Corporate Authors: United States National Aeronautics and Space Administration Scientific and Technical Information Division, United States. National Aeronautics and Space Administration., Scientific and Technical Information Division
Other Authors: Kaminer, Isaac
Format: Book
Language:English
Published: [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990
Series:NASA contractor report NASA CR-4268
Subjects:
ΒιβλιοθήκηΤαξιθετικός αριθμόςΑριθμός ΑντιτύπωνΠληροφορίεςΚατάσταση
Δημοκρίτειο Πανεπιστήμιο ΘράκηςTL 521 .31ΠροβολήOPAC