A computer program is presented for facilitating the development and assessment of flight control systems, and application to a control design is discussed. The program is a computer-aided control-system design program based on direct digital synthesis of a proportional-integral-filter controller with scheduled linear-quadratic-Gaussian gains and command generator tracking of pilot inputs. The FlightCAD system concentrates on aircraft dynamics, flight-control systems, stability and performance, and has practical engineering applications.
Computer-aided design of flight control systems
AIAA Guidance, Navigation and Control Conference ; 1991 ; New Orleans, LA, United States
1991-01-01
Conference paper
No indication
English
Computer-Aided Design of Flight Control Systems
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