JPS60181598U

JPS60181598U - Flying body rudder angle control device

Info

Publication number: JPS60181598U
Application number: JP6630584U
Authority: JP
Inventors: 亨奥田
Original assignee: 三菱電機株式会社
Priority date: 1984-05-07
Filing date: 1984-05-07
Publication date: 1985-12-02

Abstract

(57)【要約】本公報は電子出願前の出願データであるた
め要約のデータは記録されません。(57) [Summary] This bulletin contains application data before electronic filing, so abstract data is not recorded.

Description

[Brief explanation of the drawing]

第１図は従来の舵角制御装置を示すブロック図、第２図
はこの考案の一実施例を示すブロック図、第３図はこの
考案の一実施例におけるスイッチ切換えパターンを示す
図である。図において１ａ〜１ｃはロール、ピッチ、ヨーの誘導信
号、２ａ〜２ｃは第１〜第３の制御器、３ａ〜３ｃはロ
ール、ピッチ、ヨーの舵角制御信号、４は加算器、５は
舵角指令信号、６は舵駆動装置、７はタイマ、８はスイ
ッチ駆動信号、９ａ〜９ｃは第１〜第３のスイッチであ
る。なお、図中同一符号は同一または相当部分を示すも
のとする。FIG. 1 is a block diagram showing a conventional steering angle control device, FIG. 2 is a block diagram showing an embodiment of this invention, and FIG. 3 is a diagram showing a switch switching pattern in an embodiment of this invention. In the figure, 1a to 1c are roll, pitch, and yaw guidance signals, 2a to 2c are first to third controllers, 3a to 3c are roll, pitch, and yaw steering angle control signals, 4 is an adder, and 5 is an adder. A steering angle command signal, 6 a rudder drive device, 7 a timer, 8 a switch drive signal, and 9a to 9c are first to third switches. Note that the same reference numerals in the figures indicate the same or corresponding parts.

Claims

[Scope of utility model registration request]

A rudder angle control device for a flying object guided to a target while controlling roll motion includes a first controller that generates a roll rudder angle control signal from a roll guidance signal and a pitch rudder angle control signal that generates a pitch rudder angle control signal from a pitch guidance signal. a second controller that generates a yaw steering angle control signal, a third controller that generates a yaw steering angle control signal from the yaw guidance signal, and an adder that generates a steering angle command signal from the roll, pitch, and yaw steering angle control signals; A rudder drive device that drives the rudder using a rudder angle command signal, a first switch that connects a roll rudder angle control signal to an adder, a second switch that connects a pitch rudder angle control signal to an adder, and a yaw rudder. It consists of a third switch that connects the angle control signal to the adder, and a timer that generates drive signals for the first to third switches, and switches the three switches in a predetermined order according to the time set by the timer. A rudder angle control device for a flying body, characterized in that rudder angle control in each direction of roll, pitch, and yaw is performed in a time-sharing manner.