Honeywell has designed a digital self-adaptive flight control system for flight test in the VALT Research Aircraft (a modified CH-47). The final design resulted from a comparison of two different adaptive concepts: one based on explicit parameter estimates from a real-time maximum likelihood estimation algorithm and the other based on an implicit model reference adaptive system. The two designs are compared on the basis of performance and complexity.
Digital adaptive control laws for VTOL aircraft
1978 Conference on Decision and Control ; 1979 ; San Diego, CA
1979-01-01
Miscellaneous
No indication
English
Digital controllers for VTOL aircraft
Tema Archive | 1978
|AUTOLAND SYSTEM FOR VTOL AIRCRAFT, VTOL AIRCRAFT, AND LANDING CONTROL METHOD FOR VTOL AIRCRAFT
European Patent Office | 2024
|Digital controllers for VTOL aircraft
NTRS | 1976
|