JPS62201014U - - Google Patents
Info
- Publication number
- JPS62201014U JPS62201014U JP9036186U JP9036186U JPS62201014U JP S62201014 U JPS62201014 U JP S62201014U JP 9036186 U JP9036186 U JP 9036186U JP 9036186 U JP9036186 U JP 9036186U JP S62201014 U JPS62201014 U JP S62201014U
- Authority
- JP
- Japan
- Prior art keywords
- target object
- satellite
- rotating body
- detection signal
- infrared
- 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
- 238000001514 detection method Methods 0.000 claims 4
- 230000007274 generation of a signal involved in cell-cell signaling Effects 0.000 claims 2
Landscapes
- Navigation (AREA)
- 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を示す外形図、第
２図は走査線を示す図、第３図は従来の地球セン
サの走査信号を示す図である。
図中、１，９は走査線、２は地球、３は時間、
４は回転体の本体、５は回転軸、６は矢印、７は
赤外線検知器、８はスピン軸方向を示す。また、
第１図〜第３図において、同一符号は同一または
相当部分を示す。
FIG. 1 is an outline drawing showing an embodiment of this invention, FIG. 2 is a drawing showing scanning lines, and FIG. 3 is a drawing showing scanning signals of a conventional earth sensor. In the figure, 1 and 9 are scanning lines, 2 is the earth, 3 is time,
Reference numeral 4 indicates the main body of the rotating body, 5 indicates the rotation axis, 6 indicates an arrow, 7 indicates an infrared detector, and 8 indicates the direction of the spin axis. Also,
In FIGS. 1 to 3, the same reference numerals indicate the same or corresponding parts.
Claims (1)
球等の目標物に対する衛星の姿勢を検出するため
の信号を得る衛星の姿勢検知信号生成装置におい
て、目標物に対して特定の角度で対抗する平面状
の回転体と、この回転体の表面で、かつ、その回
転体の回転軸からずれた位置に固定され、目標物
からの赤外線を検知する赤外線検知器と、この赤
外線検知器による検知信号をもとにして目標物の
走査信号を生成する赤外線検出装置とで構成され
ていることを特徴とする衛星の姿勢検知信号生成
装置。 In a satellite attitude detection signal generation device that is mounted on a satellite that rotates around its spin axis and obtains a signal to detect the attitude of the satellite with respect to a target object such as the earth, a flat shape that opposes the target object at a specific angle is used. A rotating body, an infrared detector fixed on the surface of this rotating body at a position offset from the rotation axis of the rotating body to detect infrared rays from a target object, and a detection signal from this infrared detector. 1. A satellite attitude detection signal generation device, comprising: an infrared detection device that generates a scanning signal of a target object.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP9036186U JPS62201014U (en) | 1986-06-13 | 1986-06-13 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP9036186U JPS62201014U (en) | 1986-06-13 | 1986-06-13 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPS62201014U true JPS62201014U (en) | 1987-12-22 |
Family
ID=30950149
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP9036186U Pending JPS62201014U (en) | 1986-06-13 | 1986-06-13 |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS62201014U (en) |
-
1986
- 1986-06-13 JP JP9036186U patent/JPS62201014U/ja active Pending
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