JPS6365431A - Camera to be mounted on remote control aircraft - Google Patents
Camera to be mounted on remote control aircraftInfo
- Publication number
- JPS6365431A JPS6365431A JP21050686A JP21050686A JPS6365431A JP S6365431 A JPS6365431 A JP S6365431A JP 21050686 A JP21050686 A JP 21050686A JP 21050686 A JP21050686 A JP 21050686A JP S6365431 A JPS6365431 A JP S6365431A
- Authority
- JP
- Japan
- Prior art keywords
- camera
- confirmation
- polaroid
- film case
- remote control
- 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.)
- Granted
Links
- 238000012790 confirmation Methods 0.000 claims abstract description 16
- 230000001105 regulatory effect Effects 0.000 abstract description 2
- 238000003780 insertion Methods 0.000 description 4
- 230000037431 insertion Effects 0.000 description 4
- 230000000694 effects Effects 0.000 description 2
- 239000000725 suspension Substances 0.000 description 2
- 238000009434 installation Methods 0.000 description 1
- 239000003562 lightweight material Substances 0.000 description 1
- 238000000034 method Methods 0.000 description 1
Landscapes
- Cameras Adapted For Combination With Other Photographic Or Optical Apparatuses (AREA)
Abstract
Description
【発明の詳細な説明】
〈産業上の利用分野〉 ゛
本発明は従来の飛行機等に代わるリモコンヘリコプタ−
等のリモコン航空機による写真撮影で撮影対象の洩れや
カメラ振れ等のない、失敗のない状態で撮影することの
できるカメラに関するものである。[Detailed Description of the Invention] <Industrial Application Field> The present invention provides a remote control helicopter to replace conventional airplanes, etc.
The present invention relates to a camera that can take photographs with a remote-controlled aircraft such as a remote control aircraft without failures, without omitting objects to be photographed or camera shake.
〈従来の技術〉
有人の飛行機等による家屋や各種施設等の航空写真の撮
影が高価にならざるを得ない点を、高い高度からの撮影
は無理としても経費面からこれに代わり得る無線操縦に
よるヘリコプタ−や飛行機によって行なう方法が一般化
しつつある。<Prior art> Taking aerial photographs of houses, various facilities, etc. using manned airplanes, etc. is expensive, but even if it is impossible to take photographs from high altitudes, radio control can be used as a cost-effective alternative. Methods using helicopters and airplanes are becoming more common.
〈発明が解決しようとする問題点〉
しかし、無人のリモコン航空機による場合、解決しなけ
ればならない問題点が多い。例えば、航空機を如何に高
い所あるいは目的とする所迄飛ばすことができるか、撮
影対象が予定通りにカメラのフィルム面に入っているか
、また、ピン1〜や露出がうまくいっているかどうか、
リモコンヘリコプタ−において発生する振動の影響を如
何にして防ぐか、更にはリモコンヘリコプタ−の姿勢の
変化にも常にカメラを地上に向は続けるにはどうすれば
よいか、そして、そのような状態下でカメラを適当な角
度に傾斜維持させておくにはどのようにしたらよいかと
いった問題点がある。<Problems to be solved by the invention> However, there are many problems that need to be solved when using an unmanned remote control aircraft. For example, how high can the aircraft fly or to the desired destination, whether the subject to be photographed is on the film surface of the camera as planned, and whether the focus and exposure are correct.
How to prevent the effects of vibrations that occur in a remote control helicopter, and furthermore, how to keep the camera always pointing toward the ground even when the attitude of the remote control helicopter changes, and how to keep the camera facing the ground under such conditions. The problem is how to maintain the tilt at an appropriate angle.
本発明はこのような問題点のうち、撮影対象が正しくカ
メラのフィルム面に入っているか、また。The present invention solves these problems by determining whether the subject to be photographed is correctly placed on the film surface of the camera.
ピントや露出が適正であるか否かを確認でき、このこと
により無人航空機でも確実な写真が得られれるようにし
たのである。It was possible to check whether the focus and exposure were correct, and this made it possible to obtain reliable photographs even with unmanned aerial vehicles.
〈問題点を解決するための手段〉
そこで、本発明においては1本撮影用レンズ(1)と確
認用ポラロイドレンズ(2)とが取付けられた軽量カメ
ラボックス(3)を開発したのである。そのカメラボッ
クス(3)には前面に前記2個のレンズ(1) (2)
を併設すると共に、背面開口部(4) (5)には本撮
影用フィルムケース(6)と確認用ポラロイドフィルム
ケース(7)とを前記レンズからほぼ同一距離をおいて
配置し、背面蓋体(8)には支持用アングル(10)へ
の取付ブラケット(9)を設けた構造を開発したのであ
る。<Means for Solving the Problems> Therefore, in the present invention, a lightweight camera box (3) to which a single photographing lens (1) and a confirmation Polaroid lens (2) are attached has been developed. The camera box (3) has the two lenses (1) (2) on the front.
In addition, a film case for actual shooting (6) and a Polaroid film case for confirmation (7) are arranged at approximately the same distance from the lens in the rear openings (4) and (5), and the rear lid body We have developed a structure in which (8) is provided with a mounting bracket (9) to the support angle (10).
〈作用〉
このような構造のリモコン航空機搭載用カメラは背面蓋
体(8)に設けられた支持用アングル(10)への取付
ブラケット(9)等により任意な角度でカメラが維持さ
れ、カメラ振れも規制される。同時に本撮影用フィルム
ケース(6)と確認用ポラロイドフィルムケース(7)
内のフィルムを撮影することができ、その場でポラロイ
ドフィルムを現像させることにより1本撮影用フィルム
が正常に撮影されたか否かを間接的に知ることができる
作用がある。ポラロイド写真が正常であれば本撮影も正
常に撮影がなされたことになり、現像に回すことができ
るのである。<Function> The remote control aircraft-mounted camera with this structure maintains the camera at an arbitrary angle by the mounting bracket (9) to the support angle (10) provided on the rear cover (8), and prevents camera shake. is also regulated. At the same time, a film case for actual shooting (6) and a Polaroid film case for confirmation (7)
By developing the Polaroid film on the spot, it is possible to indirectly know whether or not a single photographic film has been properly photographed. If the Polaroid photo is normal, it means that the actual photo shoot was also taken normally, and it can be sent to development.
〈実施例〉 以下図面によって本発明の実施例を詳細に説明する。<Example> Embodiments of the present invention will be described in detail below with reference to the drawings.
第1図は本発明のリモコン航空機搭載用カメラの正面斜
視図であり、第2図は同側面図である。FIG. 1 is a front perspective view of a remote control aircraft-mounted camera of the present invention, and FIG. 2 is a side view of the same.
第3図は同背面分解斜視図である。第4図はリモコンヘ
リコプタ−への同カメラの搭載構造を示す斜視図である
。FIG. 3 is an exploded perspective view of the rear side. FIG. 4 is a perspective view showing the mounting structure of the camera on a remote control helicopter.
ここに示したリモコン航空機搭載用カメラは本撮影用レ
ンズ(1)と確認用ポラロイドレンズ(2)の2個のレ
ンズが軽量カメラボックス(3)の前面に併設されてい
る。これらのレンズはそれぞれ通常のレンズ同様にシャ
ッターと絞りを備えており。The remote-controlled aircraft-mounted camera shown here has two lenses, a lens for actual photography (1) and a Polaroid lens for confirmation (2), attached to the front of a lightweight camera box (3). Each of these lenses has a shutter and an aperture just like regular lenses.
従来公知のリモコン機構により同一条件でシャッターを
切ることができる一背面関口部(4) (5)には本撮
影用フィルムケース(6)と確認用ポラロイドフィルム
ケース(7)とを前記レンズからほぼ同一距離をおいて
配置している1本撮影用フィルムケース(6)は第3図
において左方の背面開口部(4)へ装着され、確認用ポ
ラロイドフィルムケース(7)は右方の背面開口部(5
)へ装着される。これらは互いに装着操作時に邪魔にな
らないように、軽量カメラボックス(3)に対して前後
にずらせて装着できるようになっている。確認用ポラロ
イドフィルムケース(7)は右方で軽量カメラボックス
(3)の背面開口部(5)へ直接スライドさせて装着で
き、本撮影用フィルムケース(6)は背面蓋体(8)の
中央差込口(20)から左方の背面開口部(4)へスラ
イドして装着できるようになっている。その装着の容易
さをもたせるために背面蓋体(8)の右方の一部が取外
し可能な分割1i(12)となっている。A film case for actual shooting (6) and a Polaroid film case for confirmation (7) are placed at the entrances on the back side (4) and (5), which allow the shutter to be released under the same conditions using a conventionally known remote control mechanism. The single shooting film case (6), which is placed at the same distance, is attached to the left rear opening (4) in Figure 3, and the confirmation Polaroid film case (7) is attached to the right rear opening. Part (5
). These can be attached to the lightweight camera box (3) by shifting them back and forth so that they do not interfere with each other during the attachment operation. The Polaroid film case (7) for confirmation can be attached by sliding it directly into the rear opening (5) of the lightweight camera box (3) on the right side, and the film case (6) for actual photography can be attached in the center of the rear lid (8). It can be installed by sliding it from the insertion port (20) to the rear opening (4) on the left. In order to facilitate the installation, a portion of the right side of the back cover (8) is formed into a removable division 1i (12).
このようなカメラは撮影対象や高度1時刻1周囲の状況
等によりリモコン航空機の下部へ任意な傾斜角をもって
又は真下に向いて取付ける必要性がある。カメラをリモ
コン航空機の下部へ航空機の傾斜や振動にかかわらず安
定かつ水平に保持するのは、第4図にみられるようなカ
メラ支持用フレーム(13)及び天秤杆(14)である
1本発明のリモコン航空機搭載用カメラにはカメラ支持
用フレーム(13)へ取付けるための機構が設けられて
いる。Such a camera needs to be installed at an arbitrary angle of inclination or directly downwards at the bottom of the remote control aircraft depending on the object to be photographed, the altitude, time, and surrounding conditions. The camera supporting frame (13) and the balance rod (14) as shown in FIG. 4 are used to hold the camera stably and horizontally at the bottom of the remote control aircraft regardless of the tilt or vibration of the aircraft. The remote-controlled aircraft-mounted camera is provided with a mechanism for attaching it to the camera support frame (13).
すなわち、カメラは前記カメラ支持用フレーム(13)
によって吊ることのできる支持用アングル(10)へ取
付けられる。そのために背面蓋体(8)には第2図にみ
られるように支持用アングル(10)への取付ブラケッ
ト(9)を設けている。取付ブラケット(9)は中程に
アングル挿通穴(11)が設けられた中央の主取付ブラ
ケット(9a)とその両側の副取付ブラケット(9b)
(9b)とからなる、副取付ブラケット(9b)には
三角形の切欠き(15)が設け゛られており、支持用ア
ングル(10)が当接してカメラを強固に保持する。こ
れらはカメラの背面に設けられているが、カメラ本体の
上面又は底面にある斜面にも2個の支持用突起(16)
(16)が設けられており、この支持用突起(16)
に設けられた吊索(23)に吊線(17)を通してカメ
ラ支持用フレーム(13)へ吊られる。カメラの吊角度
は主取付ブラケット(9a)をカメラ支持用フレーム(
13)に上端が固定された吊線(21)の端部にあるク
リップ(22)が掴む位置によって調節することができ
る。また、カメラを垂直方向すなわち真下に向いた状態
で保持することができるように、カメラ本体の上面と底
面には鉤状のフック(18) (19)が設けられてい
る。これらのフックを利用してカメラ支持用フレーム(
13)へ吊線(17)によって吊り下げることができる
。That is, the camera is mounted on the camera support frame (13).
It is attached to a support angle (10) which can be hung by. For this purpose, the rear lid (8) is provided with a mounting bracket (9) for mounting on the support angle (10), as shown in FIG. The mounting bracket (9) consists of a central main mounting bracket (9a) with an angle insertion hole (11) in the middle, and sub-mounting brackets (9b) on both sides of the main mounting bracket (9a).
A triangular notch (15) is provided in the sub-mounting bracket (9b) consisting of (9b), and the support angle (10) abuts against it to firmly hold the camera. These are provided on the back of the camera, but there are also two support protrusions (16) on the slopes on the top or bottom of the camera body.
(16) is provided, and this supporting protrusion (16)
The camera is suspended from the camera support frame (13) by passing the suspension line (17) through the suspension line (23) provided at the camera. To determine the hanging angle of the camera, connect the main mounting bracket (9a) to the camera support frame (
It can be adjusted by the gripping position of the clip (22) at the end of the hanging wire (21) whose upper end is fixed to 13). Additionally, hook-shaped hooks (18) and (19) are provided on the top and bottom surfaces of the camera body so that the camera can be held vertically, ie, facing straight down. Use these hooks to attach the camera support frame (
13) by a hanging wire (17).
以上のカメラボックス(3)は軽凰素材により軽量化す
ることはもちろんのことである。It goes without saying that the camera box (3) described above can be made lighter by using a lightweight material.
〈発明の効果〉
本発明のリモコン航空機搭載用カメラは以上のような構
造であるから、リモコン航空機へ振動等のない安定な状
態でしかも所望の傾斜角で取付けることができ、撮影し
た航空写真を現像して初めて撮影状態の良否が分るので
はなく、撮影時に現場で直ちに確認用ポラロイドフィル
ムを現像できて良否が判断できるので、失敗のない写真
撮影ができる。そのための本撮影用フィルムケースと確
認用ポラロイドフィルムケースの装填や交換が容易であ
る。<Effects of the Invention> Since the remote-controlled aircraft-mounted camera of the present invention has the above-described structure, it can be mounted on a remote-controlled aircraft in a stable state without vibrations and at a desired tilt angle, and the aerial photographs taken can be easily captured. Instead of knowing whether the photographic condition is good or bad only after it is developed, the Polaroid film for confirmation can be developed immediately on the spot at the time of photography, and the quality can be determined, so it is possible to take photographs without mistakes. For this purpose, it is easy to load and replace the film case for actual shooting and the Polaroid film case for confirmation.
第1図は本発明のリモコン航空機搭載用カメラの正面斜
視図であり、第2図は同側面図である。
第3図は同背面分解斜視回である。第4図はリモコンヘ
リコプタ−への同カメラの搭載構造を示す斜視図である
。
(1)本撮影用レンズ
(2)確認用ポラロイドレンズ
(3)軽量カメラボックス (4)(5)背面開口部(
6)本撮影用フィルムケース
(7)ポラロイドフィルムケース
(8)背面蓋体 (9)取付ブラケット(1
0)支持用アングル (11)アングル挿通穴(13
)カメラ支持用フレーム (14)天秤杆(16)支持
用突起 (18) (19)フック(20)中央
差込口
以上FIG. 1 is a front perspective view of a remote control aircraft-mounted camera of the present invention, and FIG. 2 is a side view of the same. Figure 3 is an exploded perspective view of the same back. FIG. 4 is a perspective view showing the mounting structure of the camera on a remote control helicopter. (1) Lens for actual shooting (2) Polaroid lens for confirmation (3) Lightweight camera box (4) (5) Rear opening (
6) Film case for actual shooting (7) Polaroid film case (8) Back cover (9) Mounting bracket (1
0) Support angle (11) Angle insertion hole (13
) Camera support frame (14) Take-up rod (16) Support protrusion (18) (19) Hook (20) Central insertion hole or above
Claims (1)
)とが取付けられた軽量カメラボックス(3)であって
、該カメラボックス(3)には前面に前記2個のレンズ
(1)(2)を併設すると共に、背面開口部(4)(5
)には本撮影用フィルムケース(6)と確認用ポラロイ
ドフィルムケース(7)とを前記レンズからほぼ同一距
離をおいて配置し、背面蓋体(8)には支持用アングル
(10)への取付ブラケット(9)を設けてなることを
特徴とするリモコン航空機搭載用カメラ。1 lens for shooting (1) and Polaroid lens for confirmation (2)
) is attached to the camera box (3), and the camera box (3) has the two lenses (1) and (2) on the front side, as well as the rear openings (4) and (5).
), a film case for actual shooting (6) and a Polaroid film case for confirmation (7) are placed at approximately the same distance from the lens, and a support angle (10) is placed on the rear lid (8). A remote control aircraft-mounted camera characterized by being provided with a mounting bracket (9).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP21050686A JPH0814678B2 (en) | 1986-09-06 | 1986-09-06 | Remote control aircraft mounting camera |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP21050686A JPH0814678B2 (en) | 1986-09-06 | 1986-09-06 | Remote control aircraft mounting camera |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS6365431A true JPS6365431A (en) | 1988-03-24 |
| JPH0814678B2 JPH0814678B2 (en) | 1996-02-14 |
Family
ID=16590494
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP21050686A Expired - Fee Related JPH0814678B2 (en) | 1986-09-06 | 1986-09-06 | Remote control aircraft mounting camera |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH0814678B2 (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5426476A (en) * | 1994-11-16 | 1995-06-20 | Fussell; James C. | Aircraft video camera mount |
-
1986
- 1986-09-06 JP JP21050686A patent/JPH0814678B2/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5426476A (en) * | 1994-11-16 | 1995-06-20 | Fussell; James C. | Aircraft video camera mount |
Also Published As
| Publication number | Publication date |
|---|---|
| JPH0814678B2 (en) | 1996-02-14 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |
|
| LAPS | Cancellation because of no payment of annual fees |