Response and recovery of an MRAC advanced flight control system to wake vortex encounters
= Rolling, pitching, and yawing moment coefficients due to wake vortex= Longitudinal
location of evaluation points of vortex-following aircraft= Lateral location of evaluation points
of vortex-following aircraft= Vertical location of evaluation points of vortex-following aircraft=
Wingspan of vortex-following aircraft= Area of wing, horizontal, and vertical evaluation
sections of vortex-following aircraft= Total wing area of vortex-following aircraft= Total rolling,
pitching, and yawing moment coefficients= Angle of attack induced due to the wake vortex …
location of evaluation points of vortex-following aircraft= Lateral location of evaluation points
of vortex-following aircraft= Vertical location of evaluation points of vortex-following aircraft=
Wingspan of vortex-following aircraft= Area of wing, horizontal, and vertical evaluation
sections of vortex-following aircraft= Total wing area of vortex-following aircraft= Total rolling,
pitching, and yawing moment coefficients= Angle of attack induced due to the wake vortex …
= Rolling, pitching, and yawing moment coefficients due to wake vortex= Longitudinal location of evaluation points of vortex-following aircraft= Lateral location of evaluation points of vortex-following aircraft= Vertical location of evaluation points of vortex-following aircraft= Wingspan of vortex-following aircraft= Area of wing, horizontal, and vertical evaluation sections of vortex-following aircraft= Total wing area of vortex-following aircraft= Total rolling, pitching, and yawing moment coefficients= Angle of attack induced due to the wake vortex= Lift curve slope of vortex-following aircraft
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