| 摘要 |
PROBLEM TO BE SOLVED: To provide a guided missile dispensing with setting of a wide safety zone around a firing position, and being not restrained from operations such as change of a firing direction and a flying route of the guided missile. SOLUTION: In this N stage-type guided missile, each of M-th stages (M is integer of 1 to N-1) as separated lower stages, comprises a GPS 103 detecting positional information of the guided missile, a flight computer 104 calculating a flying range of the guided missile on the basis of the positional information and flying characteristics of the guided missile, a fall point selecting computer 106 selecting a falling position within the flying range from regional information free from damage in falling, and an autopilot 107 for controlling the flight of the M-th stage after separation toward the selected falling position, and the N-th stage comprises an autopilot 207 for controlling the guided missile before separating the lower stages in the lump, and controlling the flight after separating all of the lower stages. COPYRIGHT: (C)2007,JPO&INPIT
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