JPH0387097U

JPH0387097U -

Info

Publication number: JPH0387097U
Application number: JP14961789U
Authority: JP
Priority date: 1989-12-26
Filing date: 1989-12-26
Publication date: 1991-09-04

Description

[Brief explanation of the drawing]

第１図はこの考案の一実施例による飛翔体のロ
ール系自動操縦装置を示す図、第２図は第１図に
示す実施例についてのロール系角速度指令の設定
方法を説明する図、第３図は第１図に示す実施例
について一部の機能をマイクロプロセツサで行う
実施例を示す図、第４図はこの考案の一実施例に
よる飛翔体のロール系自動操縦装置の他の実施例
を示す図、第５図は第４図に示す実施例について
のロール系角速度指令の設定方法を説明する図、
第６図は第４図に示す実施例について一部の機能
をマイクロプロセツサで行う実施例を示す図、第
７図は従来の飛翔体のロール系自動操縦装置を示
す図である。１……ロール系舵角指令計算器、２……ロール
系操舵装置、３……ロール系機体動特性、４……
ロール系角速度検出器、５……極性判定器、６…
…切替えスイツチ、７……ロール系角速度指令設
定器（十）、８……ロール系角速度指令設定器（
―）、９……設定値判定器、１０……ロール系角
速度指令設定器１、１１……ロール系角速度指令
設定器２、１２……ロール系角速度指令設定器、
１３……マイクロプロセツサである。なお、図中
、同一符号は同一、あるいは相当部分を示す。 FIG. 1 is a diagram showing a roll system autopilot system for a flying object according to an embodiment of this invention, FIG. 2 is a diagram explaining a method of setting a roll system angular velocity command for the embodiment shown in FIG. The figure shows an embodiment in which a part of the functions of the embodiment shown in FIG. 1 is performed by a microprocessor, and FIG. 4 shows another embodiment of a roll system autopilot system for a flying object according to an embodiment of this invention. FIG. 5 is a diagram illustrating a method of setting the roll system angular velocity command for the embodiment shown in FIG.
FIG. 6 is a diagram showing an embodiment in which a part of the functions of the embodiment shown in FIG. 4 is performed by a microprocessor, and FIG. 7 is a diagram showing a conventional roll system automatic pilot system for a flying object. 1...Roll system rudder angle command calculator, 2...Roll system steering device, 3...Roll system vehicle dynamic characteristics, 4...
Roll system angular velocity detector, 5...Polarity determiner, 6...
...Switchover switch, 7...Roll system angular velocity command setter (10), 8...Roll system angular velocity command setter (
-), 9...Set value determiner, 10...Roll system angular velocity command setter 1, 11...Roll system angular velocity command setter 2, 12...Roll system angular velocity command setter,
13...It is a microprocessor. In addition, in the figures, the same reference numerals indicate the same or corresponding parts.

Claims

[Scope of Claim for Utility Model Registration] (1) Means mounted on a flying object to detect the roll-based angular velocity of the flying object, means for setting a positive command for the roll-based angular velocity, and means for setting a negative command for the roll-based angular velocity. means for calculating an appropriate steering angle command from the roll system angular velocity and the roll system angular velocity command, and means for actually steering in response to the navigation angle command;
A roll system autopilot device for a flying object, comprising means for switching the polarity of a roll system angular velocity command from an initial value of a roll system angular velocity of the flying object. (2) means for setting a positive command for the roll system angular velocity, means for setting a negative command for the roll system angular velocity, and means for calculating an appropriate steering angle command from the roll system angular velocity and the roll system angular velocity command; Claim (1) of the Utility Model Registration Claim is characterized in that the means for switching the polarity of the roll system angular velocity command from the initial value of the roll system angular velocity of the flying object is executed all at once by a microprocessor. Roll system autopilot device for flying objects. (3) A means mounted on a flying object to detect the roll-based angular velocity of the flying object, a means for setting a plurality of roll-based angular velocity commands, and an appropriate steering angle command calculated from the roll-based angular velocity and the roll-based angular velocity command. means for actually steering in response to the steering angle command; and means for switching the set value of the roll-based angular velocity command from the initial value of the roll-based angular velocity of the flying object.
Roll system autopilot device for flying objects. (4) Means for setting a plurality of roll-based angular velocity commands, means for calculating an appropriate steering angle command from the roll-based angular velocity and the roll-based angular velocity command, and means for calculating the roll-based angular velocity command from the initial value of the roll-based angular velocity of the projectile. 3. A roll system automatic pilot system for a flying object as set forth in claim (3) of claim 3, wherein the means for switching the setting values are executed collectively by a microprocessor.