JPH0485196A - Deck-landing guide for helicopter and vertical take-off and landing plane - Google Patents
Deck-landing guide for helicopter and vertical take-off and landing planeInfo
- Publication number
- JPH0485196A JPH0485196A JP19630990A JP19630990A JPH0485196A JP H0485196 A JPH0485196 A JP H0485196A JP 19630990 A JP19630990 A JP 19630990A JP 19630990 A JP19630990 A JP 19630990A JP H0485196 A JPH0485196 A JP H0485196A
- Authority
- JP
- Japan
- Prior art keywords
- landing
- deck
- ship
- helicopter
- plane
- 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
- 238000010586 diagram Methods 0.000 description 3
- 238000000034 method Methods 0.000 description 2
- 238000005096 rolling process Methods 0.000 description 2
- 230000001419 dependent effect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 239000003381 stabilizer Substances 0.000 description 1
Abstract
Description
【発明の詳細な説明】
〔産業上の利用分野〕
本発明はへリコデタおよびＶＴＯＬ機（航空機）が船舶
のデツキに着艦する際の誘導装置に関する。DETAILED DESCRIPTION OF THE INVENTION [Field of Industrial Application] The present invention relates to a guidance system for use when a helicopter or VTOL aircraft (aircraft) lands on the deck of a ship.
従来ヘリコプタ等の船舶への着艦はパイロットの技量の
みに依存し、特別な誘導は行われていない。Conventionally, landing a ship such as a helicopter depends only on the pilot's skill, and no special guidance is provided.
現在、ヘリコプタ等の船舶への着艦の際には特別な誘導
が行われないため、着艦は・ダイロットの技量に依存し
ており、そのため以下のような問題を生じる。Currently, no special guidance is provided when landing on ships such as helicopters, so landing is dependent on the pilot's skill, which causes the following problems.
（１） へリコグタおよび航空機の艦上運用の範囲が
限定される。（波の荒り日には運用できない。）
（２）確実な誘導がないため、着艦に必要以上の時間が
かかる。(1) The scope of on-board operation of helicopters and aircraft will be limited. (Cannot be operated on days with rough seas.) (2) Because there is no reliable guidance, landing takes longer than necessary.
（３）パイロットが着艦技術を習得するのにかなりの訓
練時間を要する。(3) It takes a considerable amount of training time for pilots to master landing techniques.
本発明は、着艦を迅速、安全に行うことのできる着艦誘
導装置を提供することを目的とする。SUMMARY OF THE INVENTION An object of the present invention is to provide a ship landing guidance system that can quickly and safely land a ship.
本発明は、着艦デツキを有する船舶に、着艦しようとす
るヘリコプタ等の高度・距離を測定し、リアルタイムで
送信する装置を設け、また着艦するヘリコプタ等に、船
舶から送られたデータを受信する装置およびデータを表
示する装置を設けてこれにより着艦の誘導を行わせるも
のである。The present invention provides a ship with a landing deck with a device that measures the altitude and distance of a helicopter, etc. that is about to land on the ship, and transmits it in real time, and also transmits the data sent from the ship to the helicopter, etc. that is landing on the ship. A device for receiving data and a device for displaying data are provided to guide the landing.
このような誘導装置によりノ臂イロットは受信したデー
タを表示器に表示することにより、自機の着艦状態を表
示器上で見ながら着艦することができノンイロットのワ
ークロードが軽減される。また自機の位置の測定装置を
搭載する必要がないので容積、重量が節約され、また艦
船上であれば大型で重い測定装置の使用も可能である。By displaying the received data on the display using such a guidance device, the non-pilots can land while viewing the landing status of their own aircraft on the display, reducing the workload of the non-pilots. In addition, there is no need to carry a device to measure the position of the aircraft, which saves space and weight, and it is also possible to use large and heavy measuring devices onboard a ship.
本発明の誘導装置では艦船のローリング等の影響を受け
るが、ローリングは艦船にフィンスタビライザーを設け
ることにより軽減でき、デツキにステーブル・シップシ
ステムを用いればさらに有効である。Although the guidance system of the present invention is affected by the rolling of the ship, rolling can be reduced by providing a fin stabilizer on the ship, and it is even more effective if a stable ship system is used for the deck.
本発明の詳細な説明する。 The present invention will be described in detail.
第１図の実施例で説明すると、着艦デツキを有する船舶
１に着艦するヘリコプタ等２の高度・距離を測定し、リ
アルタイムで送信する装置３を設ける。またヘリコプタ
等２には、船舶から送られたデータを受信する装置４お
よびデータを表示する装置５を設ける。To describe the embodiment shown in FIG. 1, a device 3 is provided for measuring the altitude and distance of a helicopter or the like 2 landing on a ship 1 having a landing deck and transmitting the information in real time. The helicopter or the like 2 is also provided with a device 4 for receiving data sent from a ship and a device 5 for displaying the data.
第２図に示すように、着艦するヘリコプタ等の高度・距
離は、デツキの着艦地点６を基単とする。As shown in Fig. 2, the altitude and distance of the helicopter, etc. landing on the ship are based on the landing point 6 of the deck.
まな高度ｈ・距離りは、測定器からヘリコプタ等までの
距離りと測定器からヘリコプタ等への見上げ角０を測定
することによって行う。着艦デツキから測定器までの高
さをＨ１測定器から着艦地点までの水平距離をｔ′とす
ると、ｈおよびｔは以下の式によって求められる。The altitude h and distance are determined by measuring the distance from the measuring device to the helicopter, etc., and the angle 0 of looking up from the measuring device to the helicopter, etc. Assuming that the height from the landing deck to the measuring instrument is H1 and the horizontal distance from the measuring instrument to the landing point is t', h and t are determined by the following equations.
ｈ＝Ｌ−―θ＋Ｈ
ＬｇＬ−ａｓａ−Ｌ’
着艦デツキを有する艦船１から送信されたデータを着艦
するヘリコプタ等２で受信し、表示する。h=L--θ+H LgL-asa-L' Data transmitted from a ship 1 having a landing deck is received by a helicopter or the like 2 landing on the ship and displayed.
本実施例では、第３図（ａ）に示すようにＨＵＤ （ヘ
ッド・アップ・ディスグレイ）１３にヘリコプタ等位置
（高度）１４と着艦デツキ位置１５をシンデルで示し、
距離ｔをデジタル値で示す。In this embodiment, as shown in FIG. 3(a), the helicopter position (altitude) 14 and the landing deck position 15 are shown in sindels on the HUD (head up display) 13,
The distance t is shown as a digital value.
パイロットは、第３図（ｂ）Ｋ示すように自機のデツキ
に対する位置１４をＩＤ上で見ながら、自機のデツキに
対しての上下動（ヒービング）を減じるように機体を操
りながら（自機の動きを、船舶の着艦位置でのヒービン
グに合ゎせるようニ操作しながら）徐々に高度を下げて
着艦する。The pilot, while looking at the position 14 of his aircraft relative to the deck on the ID, as shown in Figure 3(b)K, maneuvers the aircraft to reduce the vertical movement (heaving) of his aircraft relative to the deck. While adjusting the aircraft's movements to match the heaving at the ship's landing position, the aircraft gradually lowers its altitude and lands.
本発明を採用することによって、ヘリコプタ等が船舶に
着艦する操作に関して・ダイロットの技量への依存度が
低くなる。ま九着艦に要する時間が短縮され、悪天候下
でのヘリコプタ等の艦上運用の範囲が拡大する。By adopting the present invention, the dependence on the pilot's skill regarding the operation of landing a helicopter or the like on a ship is reduced. The time required to land on a ship will be shortened, and the scope of onboard operations such as helicopters will be expanded in bad weather.
第１図は、本発明の詳細な説明するための概略図であり
、第２図は本発明の実施例における高度および距離の算
出方法を示す図であり、第３図は本発明の実施例におけ
るヘリコプタ等の着艦操作を示す図である。
ｉ−・・艦船、２−・・ヘリコプタ等、３・・・データ
送信装置、４・・・データ受信装置、５・・・表示装置
。
（ａ）ＨＬＪＤ（へ／ド・アップ・デイスプレィ）の表
示第３図FIG. 1 is a schematic diagram for explaining the present invention in detail, FIG. 2 is a diagram showing a method of calculating altitude and distance in an embodiment of the present invention, and FIG. 3 is a diagram showing an embodiment of the present invention. It is a figure which shows the landing operation of a helicopter etc. in . i-... Ship, 2-... Helicopter etc., 3... Data transmitting device, 4... Data receiving device, 5... Display device. (a) HLJD (head/up display) display Figure 3
Claims (1)
ＴＯＬ機の高度・距離の測定装置とその測定データを送
信する装置を設け、ヘリコプタ・ＶＴＯＬ機には前記送
信されたデータを受信しパイロットに表示する装置を設
けたことを特徴とする着艦誘導装置。Helicopter V landing on a ship with a landing deck
A landing guidance system characterized in that a device for measuring the altitude and distance of a TOL aircraft and a device for transmitting the measured data are provided, and a device for receiving the transmitted data and displaying it to the pilot is provided for the helicopter/VTOL aircraft. Device.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP19630990A JPH0485196A (en) | 1990-07-26 | 1990-07-26 | Deck-landing guide for helicopter and vertical take-off and landing plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP19630990A JPH0485196A (en) | 1990-07-26 | 1990-07-26 | Deck-landing guide for helicopter and vertical take-off and landing plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPH0485196A true JPH0485196A (en) | 1992-03-18 |
Family
ID=16355666
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP19630990A Pending JPH0485196A (en) | 1990-07-26 | 1990-07-26 | Deck-landing guide for helicopter and vertical take-off and landing plane |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH0485196A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US8669883B2 (en) | 2008-08-16 | 2014-03-11 | Qinetiq Limited | Visual landing aids |
| CN108227722A (en) * | 2017-12-28 | 2018-06-29 | 南京航空航天大学 | A kind of unmanned helicopter based on infrared vision warship guidance control method |
-
1990
- 1990-07-26 JP JP19630990A patent/JPH0485196A/en active Pending
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US8669883B2 (en) | 2008-08-16 | 2014-03-11 | Qinetiq Limited | Visual landing aids |
| CN108227722A (en) * | 2017-12-28 | 2018-06-29 | 南京航空航天大学 | A kind of unmanned helicopter based on infrared vision warship guidance control method |
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