| 摘要 |
PROBLEM TO BE SOLVED: To eliminate disadvantages in a conventional intercepter missile that the guidance performance of the intercepter missile can not be sufficiently achieved, or the wide interceptable range can not be taken, as a flight route to make the interception from the proper direction is not determined under careful consideration, besides taking particular note on the characteristic of RCS and the deceleration characteristic of an opponent missile relating to the accuracy in the guidance of the intercepter missile. SOLUTION: The flight route to make the interception from the direction of large RCS is determined on the basis of the information on the opponent missile 8 to achieve both of the improvement of the guidance performance of the interceptor missile and the enlargement of the interceptable range, and further the flight route to make the interception from the direction to reduce the influence of the decelerating/accelerating speed on the accuracy in guidance is determined on the basis of the information on the opponent missile 8, to achieve both of the improvement of the guidance performance of the interceptor missile and the enlargement of the interceptable range. COPYRIGHT: (C)2005,JPO&NCIPI
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