The design of a set of control laws for the NASA F-8 digital fly by wire research airplane is described. These control laws implement several active controls functions: maneuver load control, ride smoothing and departure boundary limiting. The criteria and methods which were used in the design of the control laws are also included. Results of linear analyses and nonlinear simulation are summarized.
Design of active controls for the NASA F-8 digital fly-by-wire airplane
01.01.1976
Aufsatz (Konferenz)
Keine Angabe
Englisch