Techniques were developed for the unified design of multimode, variable authority automatic flight-control systems for powered-lift STOL and VTOL aircraft. A structure for such systems is developed to deal with the strong nonlinearities inherent in this class of aircraft, to admit automatic coupling with advanced air traffic control, and to admit a variety of active control tasks. The aircraft being considered is the augmentor wing jet STOL research aircraft.
A formal structure for advanced automatic flight-control systems
1975-05-01
Miscellaneous
No indication
English
A formal structure for advanced automatic flight-control systems
TIBKAT | 1975
|Advanced Automatic Flight Control Systems Project
NTIS | 1993
|Flight instruments & automatic flight control systems
TIBKAT | 2004
|Automatic flight control systems
TIBKAT | 2020
|