JPS63115899U - - Google Patents
Info
- Publication number
- JPS63115899U JPS63115899U JP791987U JP791987U JPS63115899U JP S63115899 U JPS63115899 U JP S63115899U JP 791987 U JP791987 U JP 791987U JP 791987 U JP791987 U JP 791987U JP S63115899 U JPS63115899 U JP S63115899U
- Authority
- JP
- Japan
- Prior art keywords
- control device
- attitude angle
- steering signal
- external
- attitude
- 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.)
- Granted
Links
- 238000010586 diagram Methods 0.000 description 1
Landscapes
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Description
第１図は本考案の一実施例による制御系統図で
ある。
１……外部搭載物管制装置、２……姿勢角セン
サ、３……制御装置、４……アクチユエータ（操
舵面）。
FIG. 1 is a control system diagram according to an embodiment of the present invention. 1... External payload control device, 2... Attitude angle sensor, 3... Control device, 4... Actuator (steering surface).
Claims (1)
制装置と、機体の姿勢角及び角速度を検出する姿
勢角センサと、上記外部搭載物管制装置及び姿勢
角センサの信号に基づいて操舵信号を生成し出力
する制御装置と、同制御装置より出力される操舵
信号に従い機体の姿勢をコントロールするアクチ
ユエータとを具備してなることを特徴とする離着
陸引起し姿勢角制御機構。 An external payload control device that manages the loading status of external payloads, an attitude angle sensor that detects the attitude angle and angular velocity of the aircraft, and a steering signal that generates a steering signal based on the signals from the external payload control device and attitude angle sensor. What is claimed is: 1. A takeoff and landing trigger attitude angle control mechanism comprising: a control device that outputs an output; and an actuator that controls the attitude of an aircraft according to a steering signal output from the control device.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP791987U JPH0437838Y2 (en) | 1987-01-22 | 1987-01-22 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP791987U JPH0437838Y2 (en) | 1987-01-22 | 1987-01-22 |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS63115899U true JPS63115899U (en) | 1988-07-26 |
| JPH0437838Y2 JPH0437838Y2 (en) | 1992-09-04 |
Family
ID=30791822
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP791987U Expired JPH0437838Y2 (en) | 1987-01-22 | 1987-01-22 |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH0437838Y2 (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP5594996B2 (en) * | 2009-09-14 | 2014-09-24 | 三菱重工業株式会社 | Aircraft control system |
-
1987
- 1987-01-22 JP JP791987U patent/JPH0437838Y2/ja not_active Expired
Also Published As
| Publication number | Publication date |
|---|---|
| JPH0437838Y2 (en) | 1992-09-04 |
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