JPH0181499U - - Google Patents
Info
- Publication number
- JPH0181499U JPH0181499U JP1987174861U JP17486187U JPH0181499U JP H0181499 U JPH0181499 U JP H0181499U JP 1987174861 U JP1987174861 U JP 1987174861U JP 17486187 U JP17486187 U JP 17486187U JP H0181499 U JPH0181499 U JP H0181499U
- Authority
- JP
- Japan
- Prior art keywords
- acceleration
- flying
- aircraft
- acceleration command
- command
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
- 230000001133 acceleration Effects 0.000 claims description 19
- 238000010586 diagram Methods 0.000 description 5
Landscapes
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Description
第１図はこの考案の一実施例による飛しよう体
の自動操縦装置を示す図、第２図はこの考案によ
りかけられる加速度指令制限を示す図、第３図は
従来の飛しよう体の自動操縦装置を示す図、第４
図は従来の加速度指令制限を示す図である。
１は加速度指令制限器、２，４は制御指令計算
器、３はピツチ加速度検出器、５はヨー加速度検
出器、６は本考案の自動操縦装置、７は飛しよう
体、８はこの考案による加速度指令制限、９はピ
ツチ加速度指令制限、１０はヨー加速度指令制限
、１１，１２は加速度指令制限器、１３は従来の
自動操縦装置、１４は絶対値計算器である。なお
、図中同一符号は同一又は相当部分を示す。
Figure 1 is a diagram showing an automatic pilot system for a flying object according to an embodiment of this invention, Figure 2 is a diagram showing the acceleration command limit applied by this invention, and Figure 3 is a diagram showing a conventional automatic pilot system for a flying object. Diagram showing the device, No. 4
The figure is a diagram showing conventional acceleration command limitations. 1 is an acceleration command limiter, 2 and 4 are control command calculators, 3 is a pitch acceleration detector, 5 is a yaw acceleration detector, 6 is an autopilot device according to the present invention, 7 is a flying body, and 8 is according to this invention 9 is a pitch acceleration command limit, 10 is a yaw acceleration command limit, 11 and 12 are acceleration command limiters, 13 is a conventional automatic pilot device, and 14 is an absolute value calculator. Note that the same reference numerals in the figures indicate the same or equivalent parts.
Claims (1)
により飛しよう径路角を変化させ目標を追尾する
飛しよう体の自動操縦装置において、機体のピツ
チ加速度を検出する加速度検出器と、ヨー加速度
を検出する加速度検出器と、加速度指令の絶対値
と加速度指令の方向を計算する計算器と、その加
速度指令の絶対値と方向により加速度指令制限値
を変化させうる機体の加速度指令制限器と、誘導
信号と機体加速度から操舵翼あるいは推力の制御
指令を計算する計算器とを具備したことを特徴と
する飛しよう体の自動操縦装置。 In an autopilot system for a flying object that tracks a target by changing the flying path angle by controlling the steering blades or thrust while flying through space, there is an acceleration detector that detects the pitch acceleration of the aircraft, and an acceleration detector that detects the yaw acceleration. An acceleration detector, a calculator that calculates the absolute value of the acceleration command and the direction of the acceleration command, an acceleration command limiter for the aircraft that can change the acceleration command limit value depending on the absolute value and direction of the acceleration command, and a guidance signal. 1. An autopilot device for a flying body, characterized in that it is equipped with a calculator that calculates control commands for steering wings or thrust from the acceleration of the aircraft.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP1987174861U JPH0181499U (en) | 1987-11-16 | 1987-11-16 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP1987174861U JPH0181499U (en) | 1987-11-16 | 1987-11-16 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPH0181499U true JPH0181499U (en) | 1989-05-31 |
Family
ID=31466693
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP1987174861U Pending JPH0181499U (en) | 1987-11-16 | 1987-11-16 |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH0181499U (en) |
-
1987
- 1987-11-16 JP JP1987174861U patent/JPH0181499U/ja active Pending
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