A fly by wire system in the collective control system for XV-15 Tilt Rotor Research Aircraft was evaluated. The collective control system was selected because it requires a system tracking accuracy between right and left rotors of approximately 0.1%. The performance characteristics of the collectors axel provide typical axis control response data. The demonstrator is bread boarded as a dual system instead of the triplex system.
Xv-15 Tilt Rotor Fly-by-Wire Collective Control Demonstrator Development Specifications
1981
34 pages
Report
Keine Angabe
Englisch
Folding tilt rotor demonstrator feasibility study
NTRS | 1986
|Tilt Wing Demonstrator Concept Design
British Library Conference Proceedings | 2013
|