The purpose of the report is to present a flight control system design, that can be implemented by analog hardware, to be used to control an aircraft with uncertain parameters. The design is based upon the use of modern control theory. The ideas are illustrated by considering control of STOL longitudinal dynamics. (Author)
Practical Scheme for Adaptive Aircraft Flight Control Systems
1973
23 pages
Report
No indication
English
A new model-reference adaptive scheme for aircraft flight control systems
Tema Archive | 1979
|Adaptive reconfiguration scheme for flight control systems
Tema Archive | 2010
|Adaptive Flight Control for Aircraft Safety Enhancements
NTIS | 2008
|