JPS62163197U - - Google Patents
Info
- Publication number
- JPS62163197U JPS62163197U JP4933786U JP4933786U JPS62163197U JP S62163197 U JPS62163197 U JP S62163197U JP 4933786 U JP4933786 U JP 4933786U JP 4933786 U JP4933786 U JP 4933786U JP S62163197 U JPS62163197 U JP S62163197U
- Authority
- JP
- Japan
- Prior art keywords
- circuit
- generates
- command signal
- flying object
- changes
- 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 1
- 238000010586 diagram Methods 0.000 description 4
- 238000006243 chemical reaction Methods 0.000 description 2
- 230000007274 generation of a signal involved in cell-cell signaling Effects 0.000 description 1
Landscapes
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Description
第１図はこの考案の実施例を示す構成図、第２
図は補償コマンドの変換パターンの一例を示す図
、第３図は従来の姿勢制御装置で構成された姿勢
制御システムのブロツク図、第４図は外乱発生源
の一例を示す図である。
図中、１は衛星本体、２は外乱発生源、３はト
ルク発生装置、４は姿勢制御装置、５は姿勢制御
信号発生回路、６は補償コマンド発生回路、７は
姿勢センサ、８は第１スラスタ、９は第２スラス
タ、１０はコマンド変換回路、１１は温度センサ
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 configuration diagram showing an embodiment of this invention, Figure 2
3 is a diagram showing an example of a conversion pattern of a compensation command, FIG. 3 is a block diagram of an attitude control system configured with a conventional attitude control device, and FIG. 4 is a diagram showing an example of a disturbance generation source. In the figure, 1 is the satellite body, 2 is a disturbance source, 3 is a torque generator, 4 is an attitude control device, 5 is an attitude control signal generation circuit, 6 is a compensation command generation circuit, 7 is an attitude sensor, and 8 is a first 9 is a second thruster, 10 is a command conversion circuit, and 11 is a temperature sensor. Note that the same reference numerals in the figures indicate the same or equivalent parts.
Claims (1)
する外乱トルクを打消すための補償指令信号を発
生させる回路と、温度検出器と、上記補償指令信
号を温度変化に応じて変化させる回路と、上記飛
翔体の姿勢検出信号をもとに姿勢制御信号を発生
する回路とから構成され、上記外乱トルクの温度
変化に応じた制御トルク指令信号を発生すること
を特徴とした姿勢制御装置。 A circuit that is mounted on a flying object such as an artificial sanitary object and generates a compensation command signal to cancel disturbance torque acting on the flying object, a temperature detector, and a circuit that changes the compensation command signal according to temperature changes. and a circuit that generates an attitude control signal based on the attitude detection signal of the flying object, and generates a control torque command signal according to a temperature change of the disturbance torque.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP4933786U JPS62163197U (en) | 1986-04-02 | 1986-04-02 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP4933786U JPS62163197U (en) | 1986-04-02 | 1986-04-02 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPS62163197U true JPS62163197U (en) | 1987-10-16 |
Family
ID=30871696
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP4933786U Pending JPS62163197U (en) | 1986-04-02 | 1986-04-02 |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS62163197U (en) |
-
1986
- 1986-04-02 JP JP4933786U patent/JPS62163197U/ja active Pending
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