JPH0278500U - - Google Patents
Info
- Publication number
- JPH0278500U JPH0278500U JP15924488U JP15924488U JPH0278500U JP H0278500 U JPH0278500 U JP H0278500U JP 15924488 U JP15924488 U JP 15924488U JP 15924488 U JP15924488 U JP 15924488U JP H0278500 U JPH0278500 U JP H0278500U
- Authority
- JP
- Japan
- Prior art keywords
- spacecraft
- extension mechanism
- capture
- docking
- coupling
- 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
- 230000007246 mechanism Effects 0.000 claims description 12
- 230000008878 coupling Effects 0.000 claims description 3
- 238000010168 coupling process Methods 0.000 claims description 3
- 238000005859 coupling reaction Methods 0.000 claims description 3
- 238000003032 molecular docking Methods 0.000 claims 3
- 238000000034 method Methods 0.000 claims 1
Description
第１図はこの考案の１実施例を示す図、第２図
は従来の１実施例を示す図である。
図において、１は第１の宇宙機ａ、２は第２の
宇宙機ｂ、３はボールエンド、４はダンパ、５は
ばね、６は緩衝機構、７は伸展機構、８は捕獲機
構、９は結合機構、１０はセンサー、１１は演算
制御装置である。なお、図中同一符号は同一部分
を示す。
FIG. 1 shows an embodiment of this invention, and FIG. 2 shows a conventional embodiment. In the figure, 1 is a first spacecraft a, 2 is a second spacecraft b, 3 is a ball end, 4 is a damper, 5 is a spring, 6 is a buffer mechanism, 7 is an extension mechanism, 8 is a capture mechanism, 9 10 is a coupling mechanism, 10 is a sensor, and 11 is an arithmetic and control unit. Note that the same reference numerals in the figures indicate the same parts.
Claims (1)
の宇宙機とのドツキングの際に伸展する伸展機構
と、上記伸展機構の開放端と上記第２の宇宙機に
設けられ、互いに接触して連結する一組の捕獲機
構と、上記第１、第２の宇宙機の対向面にそれぞ
れ設けられ、上記一組の捕獲機構の連結後、第１
、第２の宇宙機を結合するための結合機構との備
えたドツキング装置において、宇宙機の捕獲引込
み動作中に第１の宇宙機と第２の宇宙機の相対速
度を測定するセンサー、上記センサーにより得ら
れた速度情報を処理し予め設定したドツキング動
作設定時間内に結合を終了させるべく上記伸展機
構の動作速度を算出して上記伸展機構に制御信号
を発生する演算回路とを具備したことを特徴とす
るドツキング装置。 provided in the first spacecraft, and connected to the first spacecraft and the second spacecraft.
an extension mechanism that extends when docking with the spacecraft; a pair of capture mechanisms that are provided on the open end of the extension mechanism and the second spacecraft and are connected to each other in contact with each other; The first capture mechanism is installed on the opposing surface of the second spacecraft, and after the above-mentioned pair of capture mechanisms are connected, the first
, a docking device equipped with a coupling mechanism for coupling a second spacecraft, a sensor for measuring the relative speed of the first spacecraft and the second spacecraft during capture and retraction operation of the spacecraft; and an arithmetic circuit that processes the speed information obtained by calculating the operating speed of the extension mechanism and generates a control signal to the extension mechanism in order to complete the bonding within a preset docking operation time. Features a dotting device.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP15924488U JPH0278500U (en) | 1988-12-07 | 1988-12-07 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP15924488U JPH0278500U (en) | 1988-12-07 | 1988-12-07 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPH0278500U true JPH0278500U (en) | 1990-06-15 |
Family
ID=31440285
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP15924488U Pending JPH0278500U (en) | 1988-12-07 | 1988-12-07 |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH0278500U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH02182599A (en) * | 1989-01-06 | 1990-07-17 | Natl Space Dev Agency Japan<Nasda> | Docking mechanism |
-
1988
- 1988-12-07 JP JP15924488U patent/JPH0278500U/ja active Pending
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH02182599A (en) * | 1989-01-06 | 1990-07-17 | Natl Space Dev Agency Japan<Nasda> | Docking mechanism |
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