JPH0781699A - Spacecraft mooring equipment - Google Patents

Spacecraft mooring equipment

Info

Publication number
JPH0781699A
JPH0781699A JP5225319A JP22531993A JPH0781699A JP H0781699 A JPH0781699 A JP H0781699A JP 5225319 A JP5225319 A JP 5225319A JP 22531993 A JP22531993 A JP 22531993A JP H0781699 A JPH0781699 A JP H0781699A
Authority
JP
Japan
Prior art keywords
mooring
spacecraft
flight
fixing
rope
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
Application number
JP5225319A
Other languages
Japanese (ja)
Inventor
Shinichi Mori
森  伸一
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
IHI Corp
Original Assignee
IHI Corp
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by IHI Corp filed Critical IHI Corp
Priority to JP5225319A priority Critical patent/JPH0781699A/en
Publication of JPH0781699A publication Critical patent/JPH0781699A/en
Pending legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • B64G1/22Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/64Systems for coupling or separating cosmonautic vehicles or parts thereof, e.g. docking arrangements
    • B64G1/646Docking or rendezvous systems
    • B64G1/6462Docking or rendezvous systems characterised by the means for engaging other vehicles
    • B64G1/6464Docking probes and receivers

Landscapes

  • Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Electric Cable Installation (AREA)

Abstract

PURPOSE:To moor a spacecraft safely and easily by arranging a mooring flying device which the tip of the spacecraft can be mounted on and demounted from joining both together by a rope, and joining the spacecraft by winding the rope after the mooring flying device is fixed to mooring facilities. CONSTITUTION:When a spacecraft 10 approaches a mooring equipment 30 arranged on a space station or a space factory, a mooring flying device 20 of the spacecraft 10 is separated, and a propelling device 21 is operated by an operation device 14 in a remote control system, and is flown to a fixing device 31. At this time, while confirming an image of a television camera 22 arranged on the mooring flying device 20 by an image display device 13, a posture of the mooring flying device 20 is controlled by the propelling device 21 so as to capture the fixing device 31. When the mooring flying device 20 is housed in a tie-in part 32 of the fixing device 31, a pin of a fixing part 33 is inserted in and fixed to a receiving part 26 for fixation, and afterwards, a rope 11 is wound by a winding device 12, and the spececraft 10 is approached and rejoined to the mooring flying device 20, and mooring is completed.

Description

【発明の詳細な説明】Detailed Description of the Invention

【0001】[0001]

【産業上の利用分野】本発明は、宇宙船を係留施設へ係
留する宇宙船係留設備に関する。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a spacecraft mooring facility for mooring a spacecraft to a mooring facility.

【0002】[0002]

【従来の技術】宇宙船が宇宙基地に到着し、人員を宇宙
基地へ移動させる場合、まず宇宙船を宇宙基地の係留施
設に係留する必要がある。従来、宇宙船の係留方法とし
て、図3に示すように、宇宙船10の頭部にハッチ2を
設け、このハッチ2を宇宙基地1のハッチ取合部3に接
合するよう宇宙船10を操作し、このハッチ2から乗員
が宇宙基地1へ乗り移る方法が提案されている。宇宙船
10はハッチ2をこのハッチ取合部3に接合した状態で
係留される。
2. Description of the Related Art When a spacecraft arrives at a space station and moves personnel to the space station, it is necessary to moor the spacecraft at a mooring facility of the space station. Conventionally, as a mooring method for a spacecraft, as shown in FIG. 3, a hatch 2 is provided on the head of the spacecraft 10, and the spacecraft 10 is operated so that the hatch 2 is joined to the hatch joint 3 of the space station 1. However, a method has been proposed in which passengers transfer from the hatch 2 to the space station 1. The spacecraft 10 is moored with the hatch 2 joined to the hatch joint 3.

【0003】[0003]

【発明が解決しようとする課題】上述のように宇宙船1
0のハッチ2に宇宙基地1のハッチ取合部3を接合する
ためには、宇宙船10全体を操縦士が姿勢制御し、ドッ
キングする必要があり、高度の操縦技術を必要とする。
このドッキングの際、操縦を誤ると、宇宙船10と宇宙
基地1が接触し、双方に破損を生じる恐れがある。
As described above, the spacecraft 1
In order to join the hatch joint portion 3 of the space station 1 to the hatch 2 of 0, the pilot needs to control the attitude of the entire spacecraft 10 and dock it, which requires a high degree of control technology.
If the maneuvering is mistaken during docking, the spacecraft 10 and the space station 1 may come into contact with each other, causing damage to both.

【0004】本発明は上述の問題点に鑑みてなされたも
ので、宇宙船の係留を容易にでき、係留時に宇宙基地と
の接触の恐れのない安全な宇宙船係留設備を提供するこ
とを目的とする。
The present invention has been made in view of the above problems, and an object of the present invention is to provide a safe spacecraft mooring facility that facilitates mooring of a spacecraft and does not have a risk of contact with a space station during mooring. And

【0005】[0005]

【課題を解決するための手段】上記目的を達成するた
め、係留施設に宇宙船を係留する宇宙船係留設備であっ
て、該宇宙船係留設備は、係留施設に設けられた固定装
置と、宇宙船の先端に着脱可能に接続され係留時宇宙船
より係留施設へ飛行して前記固定装置に固定される係留
飛行装置と、前記宇宙船内に設けられ、前記係留飛行装
置に結合されたロープの巻き込み巻き出しを行う巻取装
置と、前記宇宙船内に設けられ、前記係留飛行装置を前
記固定装置に誘導する操作装置と、からなり、前記係留
飛行装置は、飛行および姿勢制御用の推進装置と、前記
固定装置を検出して前記操作装置に送信する検出装置と
を備え、前記操作装置は、前記検出装置の送信データに
基づき、前記推進装置に制御指示を与えるようにする。
In order to achieve the above object, there is provided a spacecraft mooring facility for mooring a spacecraft to a mooring facility, the spacecraft mooring facility comprising: a fixing device provided in the mooring facility; A mooring flight device that is detachably connected to the tip of the ship and flies from the spacecraft to a mooring facility during mooring and is fixed to the fixing device; and a rope that is provided in the spacecraft and that is connected to the mooring flight device. A winding device for unwinding, and an operating device provided in the spacecraft for guiding the mooring flight device to the fixed device, the mooring flight device being a propulsion device for flight and attitude control, A detecting device that detects the fixed device and transmits the fixed device to the operating device, and the operating device gives a control instruction to the propulsion device based on transmission data of the detecting device.

【0006】[0006]

【作用】宇宙船が係留施設に近づくと、係留飛行装置を
切り離し発進させる。係留飛行装置は検出装置により係
留施設に設けられた固定装置を検出してそのデータを操
作装置に送信する。操作装置は、この検出データに基づ
き推進装置を制御して係留飛行装置を固定装置に誘導す
る。係留飛行装置には巻取装置からのロープが接続され
ており、飛行につれて伸びてゆくので、巻取装置により
ロープの巻き出しを行う。係留飛行装置が固定装置に到
着すると固定装置により固定される。この状態で宇宙船
は係留施設に係留された状態となる。宇宙船より乗員が
係留施設に乗り移る場合、巻取装置によりロープを巻き
取ってゆくと、宇宙船は係留飛行装置に近づいてゆき、
ついには再び合体する。この状態で係留飛行装置を通り
係留施設へ移動し、また逆に係留施設から宇宙船へ人が
乗り移る事ができる。係留状態としては宇宙船が固定装
置に固定された係留飛行装置と一体となっている第1の
状態と、宇宙船が固定装置に固定された係留飛行装置と
離れてロープで接続された第2の状態の2通りがある。
宇宙船が係留施設より離れる場合は、第1の状態で固定
装置の固定を解除して離れる場合と、第2の状態で固定
装置を解除し、巻取装置で係留飛行装置を巻き取って引
き寄せ、宇宙船と合体して離れてゆく場合の2通りがあ
る。
[Operation] When the spacecraft approaches the mooring facility, the mooring flight device is disconnected and started. The mooring flight device detects the fixed device provided in the mooring facility by the detection device and transmits the data to the operation device. The operating device controls the propulsion device based on the detected data to guide the mooring flight device to the fixed device. The rope from the take-up device is connected to the mooring flight device, and the rope is unwound by the take-up device because it extends as the flight progresses. When the mooring flight device reaches the fixing device, it is fixed by the fixing device. In this state, the spacecraft is moored to the mooring facility. When the occupant moves from the spacecraft to the mooring facility, the rope is wound up by the winding device, and the spacecraft approaches the mooring flight device.
Finally, they are united again. In this state, a person can transfer to the mooring facility through the mooring flight device, and vice versa. As for the mooring state, the first state where the spacecraft is integrated with the mooring flight device fixed to the fixing device, and the second state where the spacecraft is separated from the mooring flight device fixed to the fixing device and connected by a rope There are two types of states.
When the spacecraft moves away from the mooring facility, the fixing device is released in the first state and then released, and the fixing device is released in the second state, and the mooring flight device is taken up by the take-up device and pulled. , There are two ways to merge with a spaceship and leave.

【0007】[0007]

【実施例】以下、本発明の実施例を図面を参照して説明
する。図1は係留設備の構成と係留方法を説明する図で
ある。図2は宇宙船と係留飛行装置の乗員移動用通路の
ハッチを示す図である。宇宙船10は先端に係留飛行装
置20を着脱可能に装備する。宇宙船10内には係留飛
行装置20に接続されたロープ11の巻き取り、巻き戻
しをする巻取装置12、係留飛行装置20に設けられた
テレビカメラ22の映像を表示する画像表示装置13、
この画像表示装置13により係留飛行装置20を操作す
る操作装置14が設けられている。また係留飛行装置2
0と取り合う先端隔壁15には乗員通路用のハッチ16
が設けられている。なお、ロープ11の中には通信ケー
ブル17が一体に組み込まれ、テレビカメラ22からの
画像信号、操作装置14からの制御指示の伝送が行われ
る。
Embodiments of the present invention will be described below with reference to the drawings. FIG. 1 is a diagram illustrating a configuration of mooring equipment and a mooring method. FIG. 2 is a diagram showing a hatch of a spacecraft and a passage for passenger movement of a mooring flight device. The spacecraft 10 is detachably equipped with a mooring flight device 20 at its tip. In the spacecraft 10, a winding device 12 for winding and unwinding the rope 11 connected to the mooring flight device 20, an image display device 13 for displaying an image of a television camera 22 provided on the mooring flight device 20,
An operation device 14 for operating the mooring flight device 20 by the image display device 13 is provided. Also moored flight device 2
There is a hatch 16 for the passenger passage in the tip bulkhead 15 that engages with 0.
Is provided. A communication cable 17 is integrally incorporated in the rope 11 so that an image signal from the television camera 22 and a control instruction from the operating device 14 are transmitted.

【0008】係留飛行装置20は宇宙船10のノーズを
形成し、宇宙船10に着脱可能に結合される。推進装置
21が後部および後部側の側部に設けられ、操作装置1
4の制御指示により飛行および姿勢制御を行う。前部に
はテレビカメラ22が設けられ、係留施設30の固定装
置31を撮像し、画像表示装置13に映像を伝送する。
円筒状のトンネルアダプタ23が中心に設けられ乗員の
移動に使用される。トンネルアダプタ23の先端には係
留飛行装置20のノーズを形成するハッチ24が設けら
れ、後端にもハッチ25が設けられている。側部には固
定用受け部26を設け、固定装置31の固定部33のピ
ンと取り合う。
Mooring flight device 20 forms the nose of spacecraft 10 and is removably coupled to spacecraft 10. The propulsion device 21 is provided on the rear portion and the side portion on the rear side, and the operating device 1
Flight and attitude control are performed according to the control instruction of 4. A TV camera 22 is provided in the front part, images the fixed device 31 of the mooring facility 30, and transmits the image to the image display device 13.
A cylindrical tunnel adapter 23 is provided at the center and is used for moving an occupant. A hatch 24 that forms the nose of the mooring flight device 20 is provided at the tip of the tunnel adapter 23, and a hatch 25 is also provided at the rear end. A fixing receiving portion 26 is provided on the side portion and engages with a pin of the fixing portion 33 of the fixing device 31.

【0009】係留施設30は宇宙ステーションや宇宙工
場に設けられており、宇宙船10を係留し、乗員の乗り
降りや機材の積み込み、積み降ろしに使用される。固定
装置31は係留飛行装置20の先端部と取り合う円錐状
凹部よりなる取合部32と、固定用受け部26にピンを
挿入して固定する固定部33より構成される。取合部3
2の先端にはトンネル34が設けられ、係留飛行装置2
0のトンネルアダプタ23と接続し、通路を構成する。
トンネル34にはハッチ35が設けられ係留飛行装置2
0が固定された時、開かれる。
The mooring facility 30 is installed in a space station or a space factory, and is used for mooring the spacecraft 10 for getting on and off passengers, loading and unloading equipment. The fixing device 31 is composed of a connecting portion 32 formed of a conical concave portion that is fitted to the tip portion of the mooring flight device 20, and a fixing portion 33 that inserts and fixes a pin into the fixing receiving portion 26. Mating department 3
A tunnel 34 is provided at the tip of the mooring flight device 2.
It is connected to the tunnel adapter 23 of 0 to form a passage.
A hatch 35 is provided in the tunnel 34, and the mooring flight device 2 is used.
It is opened when 0 is fixed.

【0010】次に動作について説明する。係留設備30
に近づくと、宇宙船10では図1(a)に示すように係
留飛行装置20を切り離して、操作装置14で推進装置
21を制御して固定装置31に向けて飛行させる。係留
飛行装置20に設けられたテレビカメラ22が固定装置
31を捕らえるよう推進装置21で係留飛行装置20の
姿勢を制御し、固定装置31に向けて、画像表示装置1
3で固定装置31を確認しながら係留飛行装置を20を
操作装置14で誘導する。この場合、宇宙船10は停止
しており、係留飛行装置20の飛行距離に応じて巻取装
置12よりロープを巻き出してゆく。
Next, the operation will be described. Mooring equipment 30
As shown in FIG. 1A, in the spacecraft 10, the mooring flight device 20 is separated, and the operation device 14 controls the propulsion device 21 to fly toward the fixed device 31. The attitude of the mooring flight device 20 is controlled by the propulsion device 21 so that the television camera 22 provided in the mooring flight device 20 catches the fixing device 31, and the image display device 1 is directed toward the fixing device 31.
While checking the fixing device 31 at 3, the mooring flight device 20 is guided by the operating device 14. In this case, the spacecraft 10 is stopped, and the rope is unwound from the winding device 12 according to the flight distance of the mooring flight device 20.

【0011】次に(b)が示すように係留飛行装置20
が、固定装置31の取合部32に納まると、固定部33
のピンが固定用受け部26に挿入され固定される。次
に、巻取装置12により巻き取りを行い、宇宙船10を
係留飛行装置20に近づけてゆき、(c)に示すように
再び結合する。
Next, as shown in (b), the mooring flight device 20.
However, when it is housed in the attaching portion 32 of the fixing device 31, the fixing portion 33
Is inserted into the fixing receiving portion 26 and fixed. Next, the winding device 12 performs winding, the spacecraft 10 is brought closer to the mooring flight device 20, and the spacecraft 10 is coupled again as shown in (c).

【0012】結合が終わると、宇宙船10の先端隔壁1
5に設けられたハッチ16、係留飛行装置20のトンネ
ルアダプタ23の前後に設けられたハッチ24、25お
よび係留施設30のトンネル34に設けられたハッチ3
5を開け、乗員の下船または乗船、機器や機材の搭載や
積み降ろしが行われる。図2は宇宙船10のハッチ1
6、係留飛行装置20の先端のハッチ24、テレビカメ
ラ22の配置の状態を示す。
When the connection is completed, the tip partition wall 1 of the spacecraft 10
5, hatches 24, 25 provided before and after the tunnel adapter 23 of the mooring flight device 20, and a hatch 3 provided in the tunnel 34 of the mooring facility 30.
5 is opened, crew members disembark or board, equipment and equipment are loaded and unloaded. Figure 2 shows the hatch 1 of the spacecraft 10.
6 shows a state in which the hatch 24 at the tip of the mooring flight device 20 and the television camera 22 are arranged.

【0013】宇宙船10は、図1(b)に示すように再
び係留飛行装置10から離し、ロープ11により係留し
てもよいし、(c)に示す状態で係留してもよい。
The spacecraft 10 may be separated from the mooring flight device 10 again as shown in FIG. 1 (b) and moored by the rope 11 or may be moored in the state shown in (c).

【0014】検出装置としてテレビカメラ22を用いた
が、さらに固定装置31と係留飛行装置10の距離を検
出する距離センサを設けてもよい。また宇宙船10と係
留飛行装置20の通信はロープ11の中に組み込まれた
通信ケーブルにより行うとしたが、アンテナ等を設け無
線通信としてもよい。画像表示装置13としては、モニ
タテレビ等を用い、操作装置14としてはジョイスティ
ックなどが用いられる。
Although the television camera 22 is used as the detection device, a distance sensor for detecting the distance between the fixed device 31 and the mooring flight device 10 may be further provided. Further, although the communication between the spacecraft 10 and the mooring flight device 20 is performed by the communication cable incorporated in the rope 11, wireless communication may be performed by providing an antenna or the like. A monitor television or the like is used as the image display device 13, and a joystick or the like is used as the operation device 14.

【0015】[0015]

【発明の効果】以上の説明から明らかなように本発明
は、宇宙船の先端を着脱可能にした係留飛行装置を設
け、両者をロープで結合し、係留飛行装置を係留施設に
固定した後、ロープを巻き取り、宇宙船と結合するの
で、係留時宇宙船が保留施設と接触したりすることがな
くなり安全かつ容易に係留できる。
As is apparent from the above description, the present invention provides a mooring flight device in which the tip of a spacecraft is detachable, connects both with a rope, and fixes the mooring flight device to a mooring facility. Since the rope is wound up and connected to the spacecraft, the spacecraft does not come into contact with the holding facility at the time of mooring and can be moored safely and easily.

【図面の簡単な説明】[Brief description of drawings]

【図1】本発明の実施例の構成と係留時の動作を説明す
る図である。
FIG. 1 is a diagram illustrating a configuration of an embodiment of the present invention and an operation during mooring.

【図2】宇宙船と係留飛行装置の乗員移動用通路のハッ
チを示す図である。
FIG. 2 is a view showing hatches of a spaceship and an occupant movement passage of a mooring flight device.

【図3】従来の係留方法を示す図である。FIG. 3 is a diagram showing a conventional mooring method.

【符号の説明】[Explanation of symbols]

10 宇宙船 11 ロープ 12 巻取装置 13 画像表示装置 14 操作装置 15 先端隔壁 16,24,25,35 ハッチ 17 通信ケーブル 20 係留飛行装置 21 推進装置 22 テレビカメラ(検出装置) 23 トンネルアダプタ 26 固定用受け部 30 係留施設 31 固定装置 32 取合部 33 固定部 34 トンネル 10 Spacecraft 11 Rope 12 Winding device 13 Image display device 14 Operating device 15 Tip bulkhead 16, 24, 25, 35 Hatch 17 Communication cable 20 Mooring flight device 21 Propulsion device 22 Television camera (detection device) 23 Tunnel adapter 26 For fixing Receiving part 30 Mooring facility 31 Fixing device 32 Connecting part 33 Fixing part 34 Tunnel

Claims (1)

【特許請求の範囲】[Claims] 【請求項1】 係留施設に宇宙船を係留する宇宙船係留
設備であって、該宇宙船係留設備は、 係留施設に設けられた固定装置と、 宇宙船の先端に着脱可能に接続され、係留時宇宙船より
係留施設へ飛行して前記固定装置に固定される係留飛行
装置と、 前記宇宙船内に設けられ、前記係留飛行装置に結合され
たロープの巻き込み巻き出しを行う巻取装置と、 前記宇宙船内に設けられ、前記係留飛行装置を前記固定
装置に誘導する操作装置と、からなり、 前記係留飛行装置は、飛行および姿勢制御用の推進装置
と、前記固定装置を検出して前記操作装置に送信する検
出装置とを備え、 前記操作装置は、前記検出装置の送信データに基づき、
前記推進装置に制御指示を与えることを特徴とする宇宙
船係留設備。
1. A spacecraft mooring facility for mooring a spacecraft to a mooring facility, wherein the spacecraft mooring facility is a fixing device provided in the mooring facility, and is detachably connected to the tip of the spacecraft. When a spacecraft flies to a mooring facility from a spacecraft and is fixed to the fixing device, a winding device that is provided in the spacecraft, and that winds and unwinds a rope that is coupled to the mooring flight device, An operating device provided in the spacecraft for guiding the mooring flight device to the fixing device; the mooring flight device detecting the fixing device and a propulsion device for flight and attitude control; and the operating device. And a detection device for transmitting to, the operation device, based on the transmission data of the detection device,
Spacecraft mooring facility characterized by giving a control instruction to the propulsion device.
JP5225319A 1993-09-10 1993-09-10 Spacecraft mooring equipment Pending JPH0781699A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP5225319A JPH0781699A (en) 1993-09-10 1993-09-10 Spacecraft mooring equipment

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP5225319A JPH0781699A (en) 1993-09-10 1993-09-10 Spacecraft mooring equipment

Publications (1)

Publication Number Publication Date
JPH0781699A true JPH0781699A (en) 1995-03-28

Family

ID=16827496

Family Applications (1)

Application Number Title Priority Date Filing Date
JP5225319A Pending JPH0781699A (en) 1993-09-10 1993-09-10 Spacecraft mooring equipment

Country Status (1)

Country Link
JP (1) JPH0781699A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2011162183A (en) * 2010-02-10 2011-08-25 Astrium Gmbh Towing device for towing space navigation machine on orbit, space navigation machine and towing space navigation machine
JP2014231978A (en) * 2013-05-30 2014-12-11 株式会社Ihiエアロスペース Missile launching device
JP2020510958A (en) * 2017-02-03 2020-04-09 シグニファイ ホールディング ビー ヴィSignify Holding B.V. Maintenance of lighting equipment using unmanned vehicles

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2011162183A (en) * 2010-02-10 2011-08-25 Astrium Gmbh Towing device for towing space navigation machine on orbit, space navigation machine and towing space navigation machine
JP2014231978A (en) * 2013-05-30 2014-12-11 株式会社Ihiエアロスペース Missile launching device
JP2020510958A (en) * 2017-02-03 2020-04-09 シグニファイ ホールディング ビー ヴィSignify Holding B.V. Maintenance of lighting equipment using unmanned vehicles
US11499680B2 (en) 2017-02-03 2022-11-15 Signify Holding B.V. Servicing a luminaire with an unmanned vehicle

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