JPS6435404U - - Google Patents
Info
- Publication number
- JPS6435404U JPS6435404U JP13091587U JP13091587U JPS6435404U JP S6435404 U JPS6435404 U JP S6435404U JP 13091587 U JP13091587 U JP 13091587U JP 13091587 U JP13091587 U JP 13091587U JP S6435404 U JPS6435404 U JP S6435404U
- Authority
- JP
- Japan
- Prior art keywords
- compensator
- aircraft
- deviation
- calculates
- flight control
- 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
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 claims description 5
- 238000010586 diagram Methods 0.000 description 2
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フライトコ
ントロール装置を示す図、第２図は従来のフライ
トコントロール装置を示す図である。
１は機体、４〜６は補償器、８はセンサ。なお
、図中、同一符号は同一又は相当部分を示す。
FIG. 1 is a diagram showing a flight control device according to an embodiment of this invention, and FIG. 2 is a diagram showing a conventional flight control device. 1 is the fuselage, 4 to 6 are compensators, and 8 is a sensor. In addition, in the figures, the same reference numerals indicate the same or corresponding parts.
Claims (1)
装置において、機体周辺の大気密度Ｐと機体速度
Ｖとの積ＰＶに相当する信号を直接あるいは間接
に検出するセンサと、機体の姿勢角変化率を受け
演算処理する第１の補償器と、上記第１の補償器
の出力とフライトコントロール装置に対する指令
との偏差を演算処理する第２の補償器と、第２の
補償器の出力と機体の姿勢角変化率との偏差を演
算処理する第３の補償器とを備え、上記３つの補
償器のゲイン及び時定数を上記センサの検出する
ＰＶに相当する信号を用いて更新することを特徴
とするフライトコントロール装置。 In the flight control system of an aircraft flying in the atmosphere, there is a sensor that directly or indirectly detects a signal corresponding to the product PV of the air density P around the aircraft and the aircraft speed V, and a calculation process based on the attitude angle change rate of the aircraft. a first compensator that calculates a deviation between the output of the first compensator and a command to the flight control device; and a second compensator that calculates the deviation between the output of the first compensator and a command to the flight control device; a third compensator that calculates a deviation between the two compensators, and updates the gains and time constants of the three compensators using a signal corresponding to the PV detected by the sensor. .
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP13091587U JPS6435404U (en) | 1987-08-28 | 1987-08-28 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP13091587U JPS6435404U (en) | 1987-08-28 | 1987-08-28 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPS6435404U true JPS6435404U (en) | 1989-03-03 |
Family
ID=31386505
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP13091587U Pending JPS6435404U (en) | 1987-08-28 | 1987-08-28 |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS6435404U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US7209375B2 (en) | 2001-10-31 | 2007-04-24 | Corning Cable Systems Llc | Method and apparatus for positioning an optical fiber |
-
1987
- 1987-08-28 JP JP13091587U patent/JPS6435404U/ja active Pending
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US7209375B2 (en) | 2001-10-31 | 2007-04-24 | Corning Cable Systems Llc | Method and apparatus for positioning an optical fiber |
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