Controls design with crossfeeds for hovering rotorcraft using quantitative feedback theory
By: by Daniel J. Biezad.
Contributors: United States. National Aeronautics and Space Administration.
Series: [NASA contractor report] -- NASA CR-195765.
Publisher: National Aeronautics and Space Administration; National Technical Information Service, distributor
Published: 1994
Place of publication: [Washington, DC; Springfield, Va
Language: eng
Format: Microform
Subjects: Aircraft models; Directional stability; Dynamic response; Feedback; Flight control; Flight simulation; Helicopter control; Hovering stability; Rotary wing aircraft
Notes: Distributed to depository libraries in microfiche.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1994] 1 microfiche.