Multi-missile cooperative attack guidance law designing method
A design method and guidance law technology, applied in the field of guidance, can solve the problems of difficulty in guaranteeing the accuracy of flight time estimation and reduced accuracy, achieve broad military application prospects, and improve the effect of penetration capabilities
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[0031] The present invention will be described in detail below in conjunction with the accompanying drawings and specific embodiments.
[0032] The design idea of the collaborative guidance law design method is mainly reflected in the following two points:
[0033] First, in order to meet the requirements of the missile group reaching the target area at the same time, the average value of the missile-to-target distance of each missile at the current moment is used as the expected missile-to-target distance, and the velocity direction of each missile is controlled so that each missile is in a center of mass of the target. is the center of the sphere, and the radius is the desired projectile-to-target distance on a spherical surface, and the target is approached synchronously until the missile group enters the target area at the same time and the projectile-to-target distance is small enough to realize projectile-to-target distance coordination.
[0034] Second, when the missi...
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