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- W765482486 abstract "A nonlinear feedback control law for the F/A-18 airplane that provides time-optimal or agile maneuvering of the half-loop maneuver at high angles of attack is given. The feedback control law was developed using the mathematical approach of singular perturbations, in which the control devices considered were conventional aerodynamic control surfaces and thrusting. The derived nonlinear control law was used to simulate F/A-18 half-loop maneuvers. The simulated results at Mach 0.6 and 0.9 compared well with pilot simulations conducted at NASA." @default.
- W765482486 created "2016-06-24" @default.
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- W765482486 date "1988-12-01" @default.
- W765482486 modified "2023-09-26" @default.
- W765482486 title "High alpha feedback control for agile half-loop maneuvers of the F-18 airplane" @default.
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