JP2000211593A - Monitor system of unmanned aircraft - Google Patents

Monitor system of unmanned aircraft

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Publication number
JP2000211593A
JP2000211593A JP11019173A JP1917399A JP2000211593A JP 2000211593 A JP2000211593 A JP 2000211593A JP 11019173 A JP11019173 A JP 11019173A JP 1917399 A JP1917399 A JP 1917399A JP 2000211593 A JP2000211593 A JP 2000211593A
Authority
JP
Japan
Prior art keywords
launch
aerial vehicle
unmanned aerial
flight
camera
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
JP11019173A
Other languages
Japanese (ja)
Inventor
Tomohisa Koike
伴久 小池
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.)
NEC Corp
Original Assignee
NEC 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 NEC Corp filed Critical NEC Corp
Priority to JP11019173A priority Critical patent/JP2000211593A/en
Publication of JP2000211593A publication Critical patent/JP2000211593A/en
Pending legal-status Critical Current

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Abstract

PROBLEM TO BE SOLVED: To provide a monitor system of unmanned aircraft that can in details monitor the flight state of a launched unmanned aircraft. SOLUTION: The monitor system of unmanned aircraft comprises, at least, a launch position monitor camera 2 for photographing the state of an unmanned aircraft before the launch, a flight monitor camera 4 for photographing the state of the unmanned aircraft after the launch, and a tracking arithmetic device 6 for arithmetically tracking the unmanned aircraft on the basis of the image information the flight monitor camera 4 provides. An image pickup unit 41 or/and a turntable 42 for supporting thereon the image pickup unit 41 within the flight monitor camera 4 are controlled in operation on the basis of the arithmetic results of the tracking arithmetic device 6.

Description

【発明の詳細な説明】DETAILED DESCRIPTION OF THE INVENTION

【0001】[0001]

【発明の属する技術分野】本発明は、無人機の監視装置
に関し、特に発射時点及び発射後の飛行状況を監視する
監視装置に関するものである。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a monitoring device for an unmanned aerial vehicle, and more particularly to a monitoring device for monitoring a flight situation at the time of launch and after launch.

【0002】[0002]

【従来の技術】従来の無人機の監視装置の一例が特開平
10−138999号公報に記載されている。この公報
に記載された無人機の監視装置は、発射位置監視カメラ
及び飛行監視カメラを有し、無人機発射装置からの発射
信号を受けて2台のカメラ画像を切換表示することによ
り無人機の監視を可能としている。
2. Description of the Related Art An example of a conventional monitoring apparatus for an unmanned aerial vehicle is disclosed in Japanese Patent Laid-Open Publication No. Hei 10-138999. The monitoring device for an unmanned aerial vehicle described in this publication has a launch position monitoring camera and a flight monitoring camera, and receives and displays a switching signal between two camera images in response to a firing signal from the unmanned aerial vehicle launching device. Monitoring is possible.

【0003】これによれば、無人機の飛行位置をレーダ
により測定、表示しながら無人機をコントロールする管
制装置において、無人機の管制員が無人機の発射前後の
状況を直接目視確認することができない場合、あるいは
レーダデータによる確認をすることができない場合に、
無人機の監視をすることができる。
[0003] According to this, in a traffic control device that controls the drone while measuring and displaying the flight position of the drone with a radar, the controller of the drone can directly visually confirm the situation before and after the launch of the drone. If you can not, or if you can not confirm by radar data,
It can monitor drones.

【0004】[0004]

【発明が解決しようとする課題】しかしながら、上記の
ような従来の無人機の監視装置においては、発射後の無
人機を追尾せずに撮像しているため、無人機の発射方向
のばらつきに対応して、できるだけ長い時間監視しよう
とすると広角で撮像しなければならず、無人機の画像が
小さくなり監視しづらいという問題があった。
However, in the conventional drone monitoring apparatus as described above, since the unmanned aerial vehicle after shooting is imaged without being tracked, it is possible to cope with variations in the firing direction of the unmanned aerial vehicle. In order to monitor for as long a time as possible, it is necessary to take an image at a wide angle, and there is a problem that the image of the unmanned aerial vehicle becomes small and monitoring is difficult.

【0005】本発明の目的は、画像による追尾を実施す
ることにより、無人機発射後の飛行状況の詳細な監視を
可能にした無人機の監視装置を提供することにある。
It is an object of the present invention to provide a monitoring apparatus for an unmanned aerial vehicle that enables detailed monitoring of a flight situation after the unmanned aerial vehicle is fired by performing tracking by an image.

【0006】[0006]

【課題を解決するための手段】本発明は、上記の課題を
解決するために以下の手段をとった。すなわち、請求項
1記載の無人機の監視装置は、発射前の無人機の状況を
撮像する発射位置監視カメラと、発射後の前記無人機の
状況を撮像する飛行監視カメラと、該飛行監視カメラか
ら得られる撮像情報に基づいて前記無人機の追尾演算を
行う追尾演算装置とを少なくとも備えることを特徴とす
るものである。
The present invention employs the following means in order to solve the above-mentioned problems. That is, the monitoring device for an unmanned aerial vehicle according to claim 1, a launch position monitoring camera that captures an image of the status of the unmanned aerial vehicle before launch, a flight monitoring camera that captures the status of the unmanned aerial vehicle after launch, and the flight monitoring camera And a tracking operation device that performs a tracking operation of the unmanned aerial vehicle based on the imaging information obtained from the imaging device.

【0007】これによれば、本発明は、無人機の飛行位
置をレーダにより測定、表示しながらコントロールする
管制システムにおける、無人機の発射前および発射後の
状況を監視する監視装置において、発射後の無人機の飛
行状況を追尾しこれに係る演算を実行することで、無人
機の詳細な監視を行うこととなる。また、このことによ
り、上記演算情報に基づけば、前記飛行監視カメラに関
する適切な制御を実施することが可能となる。
According to the present invention, there is provided a monitoring system for monitoring a situation before and after launch of an unmanned aerial vehicle in a control system for measuring and displaying a flight position of the unmanned aerial vehicle with a radar and controlling the position. By tracking the flight status of the unmanned aerial vehicle and executing an operation related thereto, detailed monitoring of the unmanned aerial vehicle is performed. This also makes it possible to perform appropriate control on the flight monitoring camera based on the calculation information.

【0008】ここで「飛行監視カメラに関する適切な制
御」というとき、これを該飛行監視カメラの撮像装置に
おけるズーム、フォーカス等に係る駆動又は/及び該撮
像装置を載置する旋回台の旋回速度ないしは旋回加速度
等の動作に関する制御にあたるものとすれば、この構成
に係る装置は、本発明の目的を達するにより適当なもの
となる装置であるということがいえ(請求項2)、結
果、発射前後を問わず常に詳細な無人機の監視が可能と
なるものである。
Here, "appropriate control of the flight monitoring camera" refers to a drive related to zooming, focusing, etc. in an imaging device of the flight monitoring camera and / or a turning speed of a swivel table on which the imaging device is mounted. In the case of controlling the operation such as the turning acceleration, it can be said that the device according to this configuration is a device that is more appropriate to achieve the object of the present invention (claim 2). Irrespective of this, detailed monitoring of the drone is always possible.

【0009】[0009]

【発明の実施の形態】以下では、本発明の実施の形態に
ついて、図を参照して説明する。図1を参照すると、本
発明の一実施形態としての無人機の監視装置が示されて
いる。図において、発射装置1は発射信号を切換器8に
出力する。発射位置監視カメラ2は発射位置付近に設置
され、撮像装置21及び旋回台22を有し、画像信号を
切換器8に出力する。カメラ制御装置3は管制員によっ
て操作され、駆動信号を発射位置監視カメラ2に出力し
駆動制御する。
Embodiments of the present invention will be described below with reference to the drawings. Referring to FIG. 1, there is shown a monitoring apparatus for an unmanned aerial vehicle according to an embodiment of the present invention. In the figure, a firing device 1 outputs a firing signal to a switch 8. The launch position monitoring camera 2 is installed near the launch position, has an imaging device 21 and a swivel base 22, and outputs an image signal to the switch 8. The camera controller 3 is operated by a controller, and outputs a drive signal to the launch position monitoring camera 2 to control the drive.

【0010】飛行監視カメラ4は無人機を追尾できるよ
うな位置に設置され、撮像装置41及び旋回台42を有
し、画像信号を切換器8及び画像処理装置5に出力す
る。画像処理装置5は無人機の位置大きさ等の情報を追
尾演算装置6に出力する。追尾演算装置6は追尾監視の
ための制御信号をカメラ制御装置(制御手段)7に出力
する。カメラ制御装置7は駆動信号を飛行監視カメラ4
に出力する。切換器8は発射信号により出力画像を選択
し、表示装置9等に出力する。表示装置9は無人機の画
像を表示する。
The flight surveillance camera 4 is installed at a position where the drone can be tracked, has an imaging device 41 and a swivel table 42, and outputs an image signal to the switch 8 and the image processing device 5. The image processing device 5 outputs information such as the position and size of the drone to the tracking operation device 6. The tracking calculation device 6 outputs a control signal for tracking monitoring to the camera control device (control means) 7. The camera control device 7 transmits the drive signal to the flight monitoring camera 4
Output to The switch 8 selects an output image based on the emission signal, and outputs it to the display device 9 or the like. The display device 9 displays an image of the drone.

【0011】次に本実施形態の動作を図1を使用して説
明する。無人機の監視のために、主として発射前から発
射の瞬間を監視するための発射位置監視カメラ2及び、
主として発射直後を監視するための飛行監視カメラ4の
2台もしくはそれ以上のカメラを設置する。この、発射
位置監視カメラ2は発射位置が撮像できる発射位置付近
に設置され、可視カメラ等の撮像装置21及び旋回台2
2を有している。飛行監視カメラ4は発射直後の無人機
を追尾できる位置に設置され、可視カメラ等の撮像装置
41及び旋回台42を有している。
Next, the operation of this embodiment will be described with reference to FIG. A launch position monitoring camera 2 mainly for monitoring the moment of launch from before launch for monitoring of the drone; and
Two or more flight monitoring cameras 4 for monitoring mainly immediately after launch are installed. The launch position monitoring camera 2 is installed in the vicinity of the launch position where the launch position can be imaged.
Two. The flight monitoring camera 4 is installed at a position where the unmanned aerial vehicle immediately after the launch can be tracked, and has an imaging device 41 such as a visible camera and a swivel 42.

【0012】発射位置監視カメラ2の撮像装置21及び
飛行監視カメラ4の撮像装置41で撮像された画像は切
換器8に出力される。切換器8は無人機発射装置1から
の発射信号を受ける前は、発射位置監視カメラ2の撮像
装置21からの入力画像を表示装置9に出力する。無人
機発射装置1からの発射信号を受けた瞬間あるいは一定
時間経過後に切換器8は飛行監視カメラ4の撮像装置4
1からの入力画像を表示装置9に出力するように切り換
える。
Images captured by the imaging device 21 of the launch position monitoring camera 2 and the imaging device 41 of the flight monitoring camera 4 are output to the switch 8. The switch 8 outputs the input image from the imaging device 21 of the launch position monitoring camera 2 to the display device 9 before receiving the launch signal from the drone launch device 1. At the moment when the launch signal from the unmanned aerial vehicle launch device 1 is received or after a certain period of time, the switch 8 is operated by the imaging device 4 of the flight monitoring camera 4.
Switching is performed so that the input image from No. 1 is output to the display device 9.

【0013】発射前においては、管制員はモニタディス
プレイ等の表示装置9に表示されている無人機の画像を
見ながら、カメラ制御装置3を操作する。カメラ制御装
置3は管制員の操作に従って、カメラのズーム、フォー
カス等の駆動信号を撮像装置21に、旋回台駆動信号を
旋回台22に出力することにより、発射位置監視カメラ
2を制御し、管制員の監視したい部分の画像を提供す
る。
Before the launch, the controller operates the camera control device 3 while watching the image of the drone displayed on the display device 9 such as a monitor display. The camera control device 3 controls the launch position monitoring camera 2 by outputting a drive signal such as a zoom and focus of the camera to the imaging device 21 and a swivel drive signal to the swivel 22 in accordance with the operation of the controller. Provide an image of the part you want to monitor.

【0014】発射後においては、飛行監視カメラ4の撮
像装置41からの画像入力を受けている画像処理装置5
は追尾目標である無人機の画像を抽出し、その位置およ
び大きさ等の情報を追尾演算装置6に出力する。追尾演
算装置6はその追尾目標の情報から、追尾するために必
要な旋回角度あるいは旋回角速度を算出しカメラ制御装
置7に出力すると共に、詳細に監視するためのズーム倍
率、フォーカス調整等のカメラ制御信号もカメラ制御装
置7に出力する。カメラ制御装置7は追尾演算装置6か
ら受けた制御信号を駆動信号に変換し、カメラのズー
ム、フォーカス等の駆動信号を撮像装置41に、旋回台
駆動信号を旋回台42に出力し、飛行監視カメラ4を制
御して画像による無人機の追尾を行う。ここで、カメラ
制御装置7は旋回台42からのフィードバック信号を受
けてフィードバック制御を実施してもよい。管制員は表
示装置9に表示される、自動的に追尾され、詳細に確認
できるような大きさに調整された画像により無人機の飛
行状態を監視することができる。
After the launch, the image processing device 5 receiving an image input from the imaging device 41 of the flight monitoring camera 4
Extracts an image of the unmanned aerial vehicle, which is a tracking target, and outputs information such as its position and size to the tracking calculation device 6. The tracking calculation device 6 calculates a turning angle or a turning angular velocity required for tracking from the information of the tracking target, outputs the calculated turning angle or turning speed to the camera control device 7, and performs camera control such as zoom magnification and focus adjustment for detailed monitoring. The signal is also output to the camera control device 7. The camera control device 7 converts a control signal received from the tracking operation device 6 into a drive signal, outputs a drive signal such as a zoom and a focus of the camera to the imaging device 41, and outputs a turntable drive signal to the turntable 42, and monitors flight. The camera 4 is controlled to track the drone by the image. Here, the camera control device 7 may execute a feedback control in response to a feedback signal from the swivel 42. The controller can monitor the flight status of the unmanned aerial vehicle based on an image displayed on the display device 9 and automatically adjusted to a size that can be checked in detail.

【0015】以上説明したように、本発明においては、
画像により無人機の追尾をしているので、無人機を長時
間にわたり詳細に監視できるという効果が得られる。
As described above, in the present invention,
Since the unmanned aerial vehicle is tracked by the image, an effect that the unmanned aerial vehicle can be monitored in detail for a long time is obtained.

【0016】以下では、本発明の他の実施形態について
図2を参照して説明する。本実施形態は図1に示された
実施形態における切換器8の代わりに第二表示装置11
を加え、さらに記録装置10、第二記録装置12を加え
た点で異なる。
Hereinafter, another embodiment of the present invention will be described with reference to FIG. This embodiment is different from the embodiment shown in FIG.
And a recording device 10 and a second recording device 12 are further added.

【0017】本実施形態では、図1に示された実施形態
において発射位置監視カメラ2及び飛行監視カメラ4か
らの画像を無人機発射装置1からの発射信号によって切
り換え表示を行う代わりに、表示装置を複数台設置する
ことにより、切換を実施せず、常に両方の画像を表示す
る。管制員は表示装置9及び第二表示装置11に表示さ
れている画像を適宜監視する。また、カメラからの画像
を表示装置のみに出力するのではなく、記録装置10及
び第二記録装置12にも出力するようにし、記録装置1
0及び第二記録装置12において画像を記録する。
In this embodiment, instead of switching and displaying the images from the launch position monitoring camera 2 and the flight monitoring camera 4 by the launch signal from the unmanned aerial vehicle launching device 1 in the embodiment shown in FIG. By installing a plurality of devices, both images are always displayed without switching. The controller monitors the images displayed on the display device 9 and the second display device 11 as appropriate. In addition, the image from the camera is output not only to the display device but also to the recording device 10 and the second recording device 12, so that the recording device 1
0 and the second recording device 12 records an image.

【0018】このように、本実施形態では、切換器をな
くしているので、構成が簡単になるという効果が得られ
る。また、画像の記録ができるので後の再生、解析を可
能としている。
As described above, in the present embodiment, since the switching device is eliminated, the effect that the configuration is simplified can be obtained. Further, since images can be recorded, later reproduction and analysis are possible.

【0019】なお、上で説明した記録装置10は、図1
で示された実施形態において、切換器8に接続してもよ
い。
It should be noted that the recording apparatus 10 described above uses FIG.
May be connected to the switch 8.

【0020】[0020]

【発明の効果】以上説明したように、請求項1記載の無
人機の監視装置によれば、発射位置監視カメラ及び飛行
監視カメラを備えた監視装置において、発射後の無人機
を追尾しこれに関する演算を行う追尾演算装置が備えら
れているから、無人機の飛行状態を、その発射前後を問
わず常に詳細に監視することできる。また、請求項2記
載の無人機の監視装置は、上記効果を具現化するもっと
も適当な構成の一つであるということができる。
As described above, according to the surveillance system for an unmanned aerial vehicle according to the first aspect, in a surveillance system equipped with a launch position monitoring camera and a flight surveillance camera, the unmanned aerial vehicle after launch is tracked and related. Since the tracking calculation device for performing the calculation is provided, the flying state of the unmanned aerial vehicle can always be monitored in detail regardless of before and after its launch. Further, it can be said that the monitoring apparatus for an unmanned aerial vehicle according to the second aspect is one of the most suitable configurations for realizing the above effects.

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

【図1】 本発明の実施形態に係る無人機の監視装置の
一例を示す説明図である。
FIG. 1 is an explanatory diagram illustrating an example of a monitoring device for an unmanned aerial vehicle according to an embodiment of the present invention.

【図2】 図1とは別形態となる本発明の実施形態に係
る無人機の監視装置の一例を示す説明図である。
FIG. 2 is an explanatory diagram showing an example of a monitoring apparatus for an unmanned aerial vehicle according to an embodiment of the present invention, which is different from FIG.

【符号の説明】[Explanation of symbols]

1 無人機発射装置 2 発射位置監視カメラ 3、7 カメラ制御装置 4 飛行監視カメラ 5 画像処理装置 6 追尾演算装置 8 切換器 9 表示装置 10 記録装置 11 第二表示装置 12 第二記録装置 21 撮像装置 22、42 旋回台 41 撮像装置 REFERENCE SIGNS LIST 1 Unmanned aircraft launch device 2 Launch position monitoring camera 3, 7 Camera control device 4 Flight monitoring camera 5 Image processing device 6 Tracking calculation device 8 Switching device 9 Display device 10 Recording device 11 Second display device 12 Second recording device 21 Imaging device 22, 42 Turning table 41 Imaging device

─────────────────────────────────────────────────────
────────────────────────────────────────────────── ───

【手続補正書】[Procedure amendment]

【提出日】平成11年10月28日(1999.10.
28)
[Submission date] October 28, 1999 (1999.10.
28)

【手続補正1】[Procedure amendment 1]

【補正対象書類名】明細書[Document name to be amended] Statement

【補正対象項目名】特許請求の範囲[Correction target item name] Claims

【補正方法】変更[Correction method] Change

【補正内容】[Correction contents]

【特許請求の範囲】[Claims]

【請求項】 発射前の無人機の状況を撮像する発射位
置監視カメラと、 発射後の前記無人機の状況を撮像する飛行監視カメラ
と、 該飛行監視カメラから得られる撮像情報に基づいて前記
無人機の追尾演算を行う追尾演算装置と、 前記飛行監視カメラにおける撮像位置又は/及び該撮像
装置を載置する旋回台の動作を、前記追尾演算装置の演
算結果に基づき制御する制御手段とを備えたことを特徴
とする無人機の監視装置。
1. A launch position monitoring camera that captures an image of a situation of an unmanned aerial vehicle before launch, a flight monitoring camera that captures a status of the unmanned aerial vehicle after launch, and an image capturing information obtained from the flight monitoring camera. A tracking calculation device that performs a tracking calculation of the unmanned aerial vehicle; and a control unit that controls an imaging position of the flight monitoring camera and / or an operation of a turntable on which the imaging device is mounted based on a calculation result of the tracking calculation device. A monitoring device for an unmanned aerial vehicle, comprising:

【手続補正2】[Procedure amendment 2]

【補正対象書類名】明細書[Document name to be amended] Statement

【補正対象項目名】0006[Correction target item name] 0006

【補正方法】変更[Correction method] Change

【補正内容】[Correction contents]

【0006】[0006]

【課題を解決するための手段】本発明は、上記の課題を
解決するために以下の手段をとった。すなわち、本発明
の無人機の監視装置は、発射前の無人機の状況を撮像す
る発射位置監視カメラと、発射後の前記無人機の状況を
撮像する飛行監視カメラと、該飛行監視カメラから得ら
れる撮像情報に基づいて前記無人機の追尾演算を行う追
尾演算装置とを少なくとも備えることを特徴とするもの
である。
The present invention employs the following means in order to solve the above-mentioned problems. That is, the present invention
The monitoring device of the unmanned aerial vehicle, a launch position monitoring camera that captures the status of the unmanned aerial vehicle before launch, a flight monitoring camera that captures the status of the drone after the launch, and imaging information obtained from the flight monitoring camera A tracking calculation device for performing a tracking calculation of the unmanned aerial vehicle based on the tracking calculation device.

【手続補正3】[Procedure amendment 3]

【補正対象書類名】明細書[Document name to be amended] Statement

【補正対象項目名】0008[Correction target item name] 0008

【補正方法】変更[Correction method] Change

【補正内容】[Correction contents]

【0008】ここで「飛行監視カメラに関する適切な制
御」というとき、これを該飛行監視カメラの撮像位置に
おけるズーム、フォーカス等に係る駆動又は/及び該撮
像装置を載置する旋回台の旋回速度ないしは旋回加速度
等の動作に関する制御にあたるものとすれば、この構成
に係る装置は、本発明の目的を達するにより適当なもの
なり、この結果、発射前後を問わず常に詳細な無人機
の監視が可能となるものである。
Here, "appropriate control of the flight monitoring camera" refers to a drive related to zooming, focusing, etc. at an imaging position of the flight monitoring camera, and / or a turning speed of a swivel table on which the imaging device is mounted. Assuming that corresponds to the control of the operation of such turn acceleration, the device according to this arrangement, it becomes <br/> suitable are the the purposes of this invention, this result is always detailed drone either before or after firing Can be monitored.

Claims (2)

【特許請求の範囲】[Claims] 【請求項1】 発射前の無人機の状況を撮像する発射位
置監視カメラと、 発射後の前記無人機の状況を撮像する飛行監視カメラ
と、 該飛行監視カメラから得られる撮像情報に基づいて前記
無人機の追尾演算を行う追尾演算装置とを少なくとも備
えることを特徴とする無人機の監視装置。
A launch position monitoring camera that captures a status of the unmanned aerial vehicle before launch; a flight monitoring camera that captures a status of the unmanned aerial vehicle after launch; and A monitoring apparatus for an unmanned aerial vehicle, comprising at least a tracking operation device for performing a tracking operation of an unmanned aerial vehicle.
【請求項2】 発射前の無人機の状況を撮像する発射位
置監視カメラと、 発射後の前記無人機の状況を撮像する飛行監視カメラ
と、 該飛行監視カメラから得られる撮像情報に基づいて前記
無人機の追尾演算を行う追尾演算装置と、 前記飛行監視カメラにおける撮像装置又は/及び該撮像
装置を載置する旋回台の動作を、前記追尾演算装置の演
算結果に基づき制御する制御手段とを備えたこと特徴と
する無人機の監視装置。
2. A launch position monitoring camera that captures the situation of the unmanned aerial vehicle before launch, a flight monitoring camera that captures the situation of the unmanned aerial vehicle after launch, and the launch monitoring camera based on imaging information obtained from the flight monitoring camera. A tracking calculation device that performs a tracking calculation of an unmanned aerial vehicle, and a control unit that controls an operation of an imaging device in the flight monitoring camera and / or a turntable on which the imaging device is mounted based on a calculation result of the tracking calculation device. A monitoring device for an unmanned aerial vehicle, comprising:
JP11019173A 1999-01-27 1999-01-27 Monitor system of unmanned aircraft Pending JP2000211593A (en)

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JP11019173A JP2000211593A (en) 1999-01-27 1999-01-27 Monitor system of unmanned aircraft

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Country Link
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Cited By (5)

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JP2009202737A (en) * 2008-02-27 2009-09-10 Mitsubishi Heavy Ind Ltd Unmanned aircraft and unmanned aircraft system
JP2014104797A (en) * 2012-11-26 2014-06-09 Hitachi-Ge Nuclear Energy Ltd Indoor inspection system
CN106165388A (en) * 2015-11-25 2016-11-23 深圳市大疆创新科技有限公司 Take photo by plane with burnt control system, take photo by plane with burnt control method and aircraft
US9954599B2 (en) 2016-07-14 2018-04-24 At&T Intellectual Property I, L.P. Method and system to dynamically identify and control a UAV with emitting instruments
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Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2009202737A (en) * 2008-02-27 2009-09-10 Mitsubishi Heavy Ind Ltd Unmanned aircraft and unmanned aircraft system
JP2014104797A (en) * 2012-11-26 2014-06-09 Hitachi-Ge Nuclear Energy Ltd Indoor inspection system
CN106165388A (en) * 2015-11-25 2016-11-23 深圳市大疆创新科技有限公司 Take photo by plane with burnt control system, take photo by plane with burnt control method and aircraft
WO2017088130A1 (en) * 2015-11-25 2017-06-01 深圳市大疆创新科技有限公司 Aerial photography focus following control system, aerial photography focus following control method and aircraft
CN106165388B (en) * 2015-11-25 2018-06-12 深圳市大疆灵眸科技有限公司 It takes photo by plane with burnt control system, take photo by plane with burnt control method and aircraft
CN108377333A (en) * 2015-11-25 2018-08-07 深圳市大疆灵眸科技有限公司 With burnt remote controler, aircraft remote controler, take photo by plane with burnt control system and method
CN108377333B (en) * 2015-11-25 2020-11-06 深圳市大疆灵眸科技有限公司 Focus following remote controller, aircraft remote controller, aerial photography focus following control system and method
US9954599B2 (en) 2016-07-14 2018-04-24 At&T Intellectual Property I, L.P. Method and system to dynamically identify and control a UAV with emitting instruments
US10291314B2 (en) 2016-07-14 2019-05-14 At&T Intellectual Property I, L.P. Method and system to dynamically identify and control a UAV with emitting instruments
CN111935444A (en) * 2019-05-13 2020-11-13 丰田自动车工程及制造北美公司 System and method for generating a field of view for an unmanned aerial vehicle

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