This article proposes a type of proportional navigation law design of plane-symmetrical vehicle with terminal attack
angle constraint for over target flight. Firstly, the line of sight rotating rate and the velocity rotating rate model of the
vehicle are expressed. Then, the attitude of the vehicle is constructed by the acceleration vector requirement of
proportional navigation law. Accordingly, the guidance command uncertain issue can be avoided for plane-symmetrical
vehicle over target flight. It guarantees high precision to hit the target. The effect and efficiency of the guidance law are
shown by simulations of characteristic trajectories.
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