System identification methods for aircraft flight control development and validation
By: Mark B. Tischler.
Contributors: Ames Research Center.
Series: NASA technical memorandum -- 110369.; USAATCOM technical report -- 95-A-007.
Publisher: National Aeronautics and Space Administration, Ames Research Center; US Army Aviation and Troop Command, Aeroflightdynamics Directorate; National Technical Information Service, distributor
Published: 1995
Place of publication: Moffett Field, Calif; [Springfield, Va
Language: eng
Format: Microform
Subjects: Aircraft design.; Computerized simulation.; Control systems design.; Dynamic response.; Fixed wings.; Flight control.; Flight tests.; Mathematical models.; Performance tests.; Rotary wing aircraft.; System identification.; Vertical landing.; Vertical takeoff.
Notes: Distributed to depository libraries in microfiche.

Shipping list no.: 96-0366-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1995] 1 microfiche.