Development and evaluation in flight of adjustable system; variable feel was provided from stick position, stick rate, normal acceleration, pitching acceleration, and pitching velocity; operation was satisfactory and illustrated effects of large amounts of response feel on stability of controlfree aircraft and control system response.
Longitudinal control feel system for in-flight research on response feel
NASA -- Tech Note
1961
31 pages
Aufsatz (Zeitschrift)
Englisch
© Metadata Copyright Elsevier B. V. All rights reserved.
Effects of control-feel configuration on airplane longitudinal control response
Engineering Index Backfile | 1961
|