JPH0314599U

JPH0314599U -

Info

Publication number: JPH0314599U
Application number: JP7210889U
Authority: JP
Priority date: 1989-06-20
Filing date: 1989-06-20
Publication date: 1991-02-14

Description

[Brief explanation of drawings]

第１図〜第６図はこの考案の飛行体の自動操縦
装置の一実施例を示す図、第７図は従来の飛行体
の自動操縦装置を示す図である。１……ピツチ加速度補償器２、２……ピツチ角
速度補償器２、６……ピツチ角速度計、７……ピ
ツチ加速度計、８……ヨー加速度補償器２、９…
…ヨー角速度補償器、１３……ヨー角速度計、１
４……ヨー加速度計、１５……ロール角速度補償
器２、１８……ロール角速度計、１９……動圧推
定器、２０……飛行体の自動操縦装置、２１……
正弦波発生器、２２……ランダム信号発生器であ
る。なお、図中、同一符号は同一又は相当部分を
示す。 1 to 6 are diagrams showing an embodiment of the automatic pilot system for an aircraft of this invention, and FIG. 7 is a diagram showing a conventional automatic pilot system for an aircraft. 1... Pitch acceleration compensator 2, 2... Pitch angular velocity compensator 2, 6... Pitch angular velocity meter, 7... Pitch accelerometer, 8... Yaw acceleration compensator 2, 9...
... Yaw angular velocity compensator, 13... Yaw angular velocity meter, 1
4...Yaw accelerometer, 15...Roll angular velocity compensator 2, 18...Roll angular velocity meter, 19...Dynamic pressure estimator, 20...Autopilot device of aircraft, 21...
Sine wave generator, 22...Random signal generator. 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 for detecting pitch angular velocity, means for detecting pitch acceleration, means for calculating pitch angular velocity command from this acceleration and pitch acceleration command, and pitch angular velocity of the flying object. A means for calculating a pitch steering angle command from the command and a pitch angular velocity, a means for detecting a yaw angular velocity, a means for detecting a yaw acceleration, a means for calculating a yaw angular velocity command from the yaw acceleration and the yaw acceleration command, Means for calculating a yaw steering angle command from an angular velocity command and a yaw angular velocity; means for detecting a roll angular velocity; means for calculating a roll steering angle command from a roll angular velocity command and a roll angular velocity; An automatic pilot system for an aircraft, characterized by comprising means for estimating dynamic pressure from roll angular velocity. (2) Means for detecting the pitch angular velocity of the flying object, means for detecting the pitch acceleration, means for calculating the pitch angular velocity command from the pitch acceleration and the pitch acceleration command, and means for calculating the pitch angular velocity command from the pitch angular velocity command and the pitch angular velocity. means for calculating an angular command; means for detecting a yaw angular velocity; means for detecting a yaw acceleration; means for calculating a rudder angle command, means for detecting a roll angular velocity, means for calculating a roll rudder angle command from the roll angular velocity command and the roll angular velocity, and estimating dynamic pressure from the roll rudder angle command or the roll rudder angle and the roll angular velocity. What is claimed is: 1. An automatic pilot system for an aircraft, characterized by comprising means for generating a sine wave signal and means for generating a sine wave signal. (3) Means for detecting the pitch angular velocity of the flying object, means for detecting the pitch acceleration, means for calculating the pitch angular velocity command from the pitch acceleration and the pitch acceleration command, and means for calculating the pitch angular velocity command from the pitch angular velocity command and the pitch angular velocity. means for calculating an angular command; means for detecting a yaw angular velocity; means for detecting a yaw acceleration; means for calculating a rudder angle command, means for detecting a roll angular velocity, means for calculating a roll rudder angle command from the roll angular velocity command and the roll angular velocity, and estimating dynamic pressure from the roll rudder angle command or the roll rudder angle and the roll angular velocity. What is claimed is: 1. An automatic pilot system for an aircraft, characterized by comprising means for generating a random signal and means for generating a random signal.