| 摘要 |
<p>PURPOSE:To permit the change of an objective splashdown point as well as the angle of incidence even after launching by a method wherein the title device is provided with an estimated flight route operating device, operating the optimum flight route, the separating attitude angle at which a payload is released and the like until a missile arrives at an intermediate point and correcting the operation by receiving a corrected objective splashdown point command from a data link device. CONSTITUTION:The title device is provided with an estimated flight route operating device 4, operating the optimum flight route, a circular cource around the intermediate point and the attitude angle at which a payload is released in accordance with the objective splashdown point of the payload and correcting the operation by receiving a corrected objective splashdown point command from a data link device 5. A steering amount setting device 3 receives the outputs of an inertia device 2 and the estimated flight route operating device 4 and transmits the amount of steering to a steering device 6 by setting it from the difference between the outputs while a releasing signal is sent to a releasing device 7 when the attitude angle has become the payload releasing attitude angle. The steering of a missile is effected by the steering device 6 by receiving the output from the amount-of-steering setting device 3 while the payload is releasing by the releasing device 7.</p> |
