JPH0262299U - - Google Patents

Description

[Brief explanation of drawings]

FIG. 1 is a system diagram of a missile wing control device according to an embodiment of this invention, and FIG. 2 is a system diagram of a conventional wing control device. In the figure, 1 is a storage unit, 2 is a trigger detector, 3 is a timer, 4 is a blade drive unit, 5 is a blade, 6 is a switch change judge, 7 is a first switch, and 8 is a second switch. . In each figure, the same reference numerals indicate the same or corresponding parts.

Claims (1)

[Scope of utility model registration request] A storage section that stores the electric charge of the direction correction signal input from the fire direction device to direct the missile to the expected meeting point with the target after launch, and a firing trigger from the fire direction device is detected and the charge in the storage section is released. The trigger detector and the reception of the target reflected signal turn on the guidance signal generated by the missile itself a certain time after launch in order to guide the missile toward the target direction.
For missiles equipped with a timer that controls the direction of the missile, a wing drive section that drives the wings of the missile based on a direction correction signal or guidance signal, and a wing that ultimately determines the direction in which the missile will fly, fire command is used when the target angular velocity is high. a switch switching determiner that determines switching of the first and second switches based on a mode switching command generated by the device and a lock-on signal of the missile itself; a first switch that shoots a timer; and a second switch that disables a direction correction signal. A wing control device characterized by being equipped with a switch.