| 摘要 |
<P>PROBLEM TO BE SOLVED: To provide navigation for preventing speed loss which is generated during initial and middle guidance and caused by course correction associated with that a missile takes a route where the missile comes close to a prediction intercept point (hereafter, PIP) from a side against a prediction route of a target, and thereby the PIP varies due to a speed change of the target. <P>SOLUTION: A guiding device includes a database where information (such as a speed of the missile at each PIP) which is estimated in a simulation in advance and being on action of coping with the high-speed moving target is stored. In the guiding device, the database is used to be allowed to select navigation that the speed loss of the missile is reduced and the turning performance is excellent in accordance with the PIP obtained by calculations (the navigation for coping with conventional navigation or counter-parallel navigation). <P>COPYRIGHT: (C)2013,JPO&INPIT |
