Variable-camber systems integration and operational performance of the AFTI/F-111 mission adaptive wing
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accumulated hours adaptive wing system aerodynamic AFCS AFTI/F-111 mission adaptive aircraft analytical approximately automode basic braked camber components control segments damping ratio direct current enhancement and gust error signal feedback Figure 17 flap Flight 26 flight control system flight testing fly-by-wire frequency responses frequency sweep function Gear ratio given in reference ground tests gust alleviation hinge moment torques Hp HU Hp Pn's hr of ground hydraulic power hydraulic systems Hysteresis impact pressure in-lb Inboard loop LVDT's LVDTs Hp major failures MAW system maximum ME/GA mode mechanical system MFCS Midspan mission adaptive wing NASA natural frequency outboard flaperon PDU motor peak-to-peak phase Pn's HU power drive units predictions pressure equalization pressure gain primary and backup primary and utility primary system rotary actuators servoactuating system servovalve step input supply pressure system operation torque loads trailing-edge transient response utility hydraulic valve variable-camber wing