Flight-test program conducted with helicopter having power control system to determine what control forces would be desirable for various modes of flight; six different configurations were evaluated; evaluation was purely qualitative, made up of opinion of eight research pilots; feel spring of 1/2 lb/in. and bobweight of 14 lb/g provided desirable control feel forces.
Flight evaluation of several spring force gradients and bobweight in cyclic-power-control system of light helicopter
NASA -- Tech Note
1960
9 pages
Report
Englisch
© Metadata Copyright Elsevier B. V. All rights reserved.
Model helicopter flight control
Tema Archiv | 2009
|Integrated Helicopter Flight Control
NTIS | 1976
|