JPH0221497U

JPH0221497U -

Info

Publication number: JPH0221497U
Application number: JP9428288U
Authority: JP
Priority date: 1988-07-16
Filing date: 1988-07-16
Publication date: 1990-02-13

Description

[Brief explanation of drawings]

第１図はこの考案の一実施例による飛しよう体
のオートパイロツト装置の概略ブロツク図、第２
図が従来のオートパイロツト装置の概略ブロツク
図である。図中１はロールコマンド、２はコント
ローラ、３はロール舵角指令信号、４は操舵サー
ボ装置、５は舵角、６は機体伝達関数、７はロー
ル角速度、８はロール加速度、９は角速度センサ
、１０は加速度センサ、１１は可変パラメータコ
ントロール、１２はセンサ、１３はメモリ回路１
、１４はメモリ回路２、１５，１６は補正信号、
１７は角速度センサ信号、１８は加速度センサ信
号である。なお、図中、同一符号は同一、又は相
当部分を示す。 Figure 1 is a schematic block diagram of an autopilot device for a flying vehicle according to an embodiment of this invention;
The figure is a schematic block diagram of a conventional autopilot device. In the figure, 1 is the roll command, 2 is the controller, 3 is the roll steering angle command signal, 4 is the steering servo device, 5 is the steering angle, 6 is the aircraft transfer function, 7 is the roll angular velocity, 8 is the roll acceleration, and 9 is the angular velocity sensor , 10 is an acceleration sensor, 11 is a variable parameter control, 12 is a sensor, 13 is a memory circuit 1
, 14 is the memory circuit 2, 15 and 16 are correction signals,
17 is an angular velocity sensor signal, and 18 is an acceleration sensor signal. In addition, in the figures, the same reference numerals indicate the same or equivalent parts.

Claims

[Scope of utility model registration request]

In the autopilot system of a flying vehicle,
A variable parameter controller that performs control compensation to achieve predetermined characteristics, and a rudder angle command signal output from the controller are input, and the steering blade is controlled to have a rudder angle of the same magnitude as the rudder angle command signal. a steering servo device; an angular velocity sensor that receives the rudder angle output from the steering servo device as an input and detects the roll angular velocity of the flying body based on an output having a flying body transmission characteristic; and an acceleration sensor that detects acceleration. A closed loop is constructed by a sensor that detects the dynamic pressure and altitude during flight as command signals for the variable parameter controller, and a sensor that uses the sensor output as input to call out the controller parameters, and also uses the best angular velocity sensor signal and acceleration. An autopilot device for a flying vehicle, characterized by comprising two memory circuits for detecting sensor signals.