Guidance law for simultaneously attacking static target by multiple missiles based on proportional guidance law
A proportional guidance, multi-missile technology, applied in the field of guidance law, can solve problems such as limited time control, and achieve the effect of easy implementation and simple structure
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[0045] The guidance law of the multi-missile attacking static target based on the proportional guidance law of the present invention, the steps are as follows:
[0046] Step 1: In the expression (1) of the remaining flight time of the missile, since the attacked target is a static target, the proportional coefficient N0 can be taken as 3, so Can be expressed as:
[0047]
[0048] In order to achieve the consistency of the whole projectile group, through such as image 3 The inter-missile network shown, each missile transmits the remaining flight time to the missile that has a network connection relationship with itself The consistency deviation is calculated by formula (2):
[0049]
[0050] where N i is the adjacent ammunition quantity set of the i-th missile, a ij is the connectivity coefficient, if the i-th missile can receive information from the j-th missile, then a ij =1, otherwise it is 0, there is no self-loop, that is, a ii =0.
[0051] Step 2: Judge th...
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