JPH0449794U - - Google Patents

Description

[Brief explanation of the drawing]

FIG. 1 is a system diagram of a flying object according to an embodiment of this invention, and FIG. 2 is a system diagram of a conventional flying object. In the figure, 1 is an antenna, 2 is an antenna angle detector, 3 is a signal processor, 4 is a wing drive device, 5 is a wing, 6
is a capacitor, 7 is a switch, 8 is a timer, 9 is a differentiator, 10 is a comparator, and 11 is an OR circuit. It should be noted that the same or equivalent parts in the drawings are designated by the same reference numerals.

Claims (1)

[Scope of utility model registration request] an antenna for tracking a target; an antenna angle detector for detecting a directivity angle of the antenna;
A signal processor that takes into account the antenna angle signal etc. from the antenna angle detector and outputs a steering signal by performing guidance control calculations, a wing drive device that drives the wings based on the steering signal, and a wing drive device that drives the wings to fly. Select the wings that control the body posture, the capacitor that stores the initial direction correction signal from the mother aircraft during launch, and whether the steering signal to the wing drive device should be from the signal processor or the capacitor. A switch that differentiates the angle signal from the antenna angle detector, a differentiator that differentiates the angle signal from the antenna angle detector, and a differentiator that compares whether the signal from the differentiator is above or below a certain level, and outputs a switch drive signal if it is above a certain level. A comparator, a timer that outputs a switch drive signal after a certain period of time from firing, and an O that transmits the switch drive signal from the comparator and timer to the switch.
A flying object characterized by being equipped with an R circuit.