Target non-escape area reliable prediction method adapting to collaborative task planning
A prediction method and mission planning technology, applied in defense devices, offensive equipment, etc., can solve problems such as the short flight time of missiles, the inability to solve the problem of target escape probability during multi-bomb coordinated attacks, and the ability of missiles to attack targets that cannot pass artificial regulations.
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[0033] The present invention will be further elaborated below by describing a preferred specific embodiment in detail in conjunction with the accompanying drawings.
[0034] Such as figure 1 As shown in , a method for reliable prediction of target no-escape zone adapted to cooperative mission planning includes the following steps:
[0035] Step 1: Select at least 2 feature points in the missile flight envelope;
[0036] According to the known missile flight envelope, N feature points in the missile flight airspace are selected according to the altitude, velocity, ballistic inclination angle, ballistic deflection angle, and thrust variation interval, and are recorded in the form of missile position vector and velocity vector.
[0037] The initial state information of feature points is determined according to the following feature vectors:
[0038] u i =[H i ,V i ,θ i ,ψ vi ,P i ] T
[0039]
[0040]
[0041] In the formula, U i Indicates the ith eigenvector in...
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