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For the forth generation fighter aircraft, with thrust vector is one of the key technique characters. In condition of High AOA (Angle of attack), the general effectors lose the maneuver efficiency or get poorly, so new type of control law must be found. This control law should not only overcome those problems but also satisfy requirements of the forth generation aircraft. So linearization method at...
Linearization method at sampling point and receding horizon optimal control is brought forward for a class of affine nonlinear system, The stability and convergence for this algorithm is proved, , therefore this algorithm can be proved to solve the stability and convergence problem of a class of affine nonlinear system through simulation of aircraft movement equation.
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