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Fig. 2

Longitudinal and pitch nonlinear optimal MCA


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: aircraft acceleration; : pilot’s head vestibule acceleration in simulator; : acceleration after nonlinear scaling & limiting; PS: pilot station; LSI: transformation matrix from simulator into inertial frame; TS: transformation matrix from angular velocity to Euler angle rates; : angular velocity after TS; : angular velocity after nonlinear scaling & limiting; : washout angular velocity after tilt rate limit; : the sum of washout angular velocity; : washout angular displacement; s: Laplace variable; : washout acceleration in the inertial frame; : washout velocity in the inertial frame; SI: washout displacement in the inertial frame; K(α): the feedback matrix

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