Optimization of VTOL control concepts with and without stabilization compared with six degree of freedom motion simulator, noting system failure effects and nonlinear concepts
VTOL control system studies on a six-degree- of-freedom motion simulator.
CONGRESS OF THE AEROSPACE PROCEEDINGS 1966 ; 1966 ; LONDON, United Kingdom
1967-01-01
Aufsatz (Konferenz)
Keine Angabe
Englisch