Program used subsonic jet propelled fighter aircraft to investigate capabilities of normal acceleration command control system, pitch rate command control system, and pitch damper system; with given stability characteristics pilots doubted that any type of military mission could be accomplished; it was found that with any of three systems flying qualities were definitely superior to those of basic aircraft.
Flight investigations of automatic stabilization of airplane having static longitudinal instability
NASA -- Tech Note
1959
32 pages
Report
English
© Metadata Copyright Elsevier B. V. All rights reserved.
Automatic flight and airplane stability
Engineering Index Backfile | 1944
|Engineering Index Backfile | 1947
|