A flight-test and simulation evaluation of the longitudinal final approach and landing performance of an automatic system for a light wing loading STOL aircraft equipped with wing spoilers
By: Stuart C. Brown, Gordon H. Hardy, and William S. Hindson
Contributors: Hardy, Gordon H; Hindson, W. S; United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch
Series: NASA technical memorandum -- 85873
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Branch
Published: 1984
Place of publication: [Washington, D.C.?]
Language: eng
Format: Microform
Subjects: Instrument landing systems; Landing aids (Aeronautics)
Notes: "N84-32393"--Microfiche header

Bibliography: p. 14

Microfiche. [Washington, D.C.? : National Aeronautics and Space Administration, 1984]. 1 microfiche ; 11 x 15 cm