521153 A7 B7 8 444twf. doc/00 9 五、發明說明（/ ) 本發明是有關於一種航空器追蹤技術。特別是關於一 種航空器視訊數據即時傳送自動追蹤系統。 (請先閱讀背面之注意事項再填寫本頁) 航空器，於現今日常生活中，是大眾所熟悉的交通’ 運輸，空中偵查之工具，其可包括各種不同型號的客機’ 貨機與軍用機等等。當其他通訊科技也同時快速發展之 際，也允許航空器有一些通訊設備，以利與控管中心之間 的聯絡。也利於控管中心對航空器的掌控。 當航空器飛上天空，進行一任務，例如載運乘客由第 處到第二處，又或是進行一地面偵查任務，其與地面聯絡 的是靠無線信號傳輸的方式進行。一般飛行員隨時回報其 所在的位置及高度等資料給地面的控制中心，以掌握航空 器的位置，及其飛行途徑。然而，可能由於飛行員的疏失， 無法將正確的資訊回報給地面的控制中心，因此造成許多 誤差，進而造成事故，或是航空器因突發事故而失去聯絡。 則航空器的所在位置與其航空器上發生的狀況，將無法獲 經濟部智慧財產局員工消費合作社印製521153 A7 B7 8 444twf.doc / 00 9 V. Description of the Invention (/) The present invention relates to an aircraft tracking technology. In particular, it relates to an automatic tracking system for real-time transmission of aircraft video data. (Please read the precautions on the back before filling out this page) Aircraft, in today's daily life, is a transportation, transportation, and air reconnaissance tool familiar to the public. It can include various types of passenger aircraft, cargo aircraft and military aircraft, etc. . While other communication technologies are also developing rapidly, aircraft are also allowed to have some communication equipment to facilitate communication with the control center. It also helps the control center to control the aircraft. When the aircraft flies into the sky, a task is carried out, such as carrying passengers from the first place to the second place, or a ground reconnaissance mission. The communication with the ground is performed by means of wireless signal transmission. Generally, pilots report their position and altitude information to the ground control center at any time to grasp the position of the aircraft and its flight path. However, due to the negligence of the pilot, the correct information cannot be reported to the control center on the ground, which results in many errors, which may cause an accident, or the aircraft may lose contact due to an unexpected accident. The location of the aircraft and the conditions on the aircraft will not be printed by the Consumer Cooperative of the Intellectual Property Bureau of the Ministry of Economic Affairs
由於目前的無線通訊得技術以高度發展，又配合另一 種全球位系統（global positioning system，GPS)或是 GLONASS定位技術。航空器上若設置有GPS、GLONASS 雙頻感測元件，航空器對應於地面的位置可準確自動偵 測，傳送給地面控制中心。然而對整個操作系統而言，並 沒有一套完整的航空器自動追蹤系統。 另外，目前航空器上的設備設計，也無法即時傳送視 訊數據資料給地面控制中心，目前僅能傳送語音資料。特 3 本紙張尺度適用中國國家標準（CNS)A4規格（210 x 297公釐） 經濟部智慧財產局員工消費合作社印製 521153 A7 8 4 44twf. doc/009 五、發明說明（V ) 別是，地面控制中心無法直接控制航空器，獲得視訊資料。 特別是當航空器上發生緊急狀況或劫機時，地面控制 中心無法主動控制航空器上的視訊設備，以掌握航空器上 的實際狀況。 目前傳統技術上，對航空器的追蹤與狀況安全監控仍 沒有一套完整有效的自動追蹤系統，可以有效偵測追蹤航 空器的路徑與其現場發生的狀況。 有鑑於此，本發明提供一種航空器視訊數據即時傳送 自動追蹤系統，得以對災害即時將影音數據資料下傳給地 面中心。另外也可利用於環保，交通，海岸巡防等，即時 將影音數據資料下傳給地面中心。又可適用於國軍立體作 戰的戰場狀況，商用客機機艙發生緊急狀況時或劫機時啓 動。又可進行高空空照。又可利於配合地面控制中心，建 立自動追蹤航空器的系統。 本發明提供一種航空器視訊數據即時傳送自動追蹤 系統，可藉由視訊與數據資料之上傳與下傳，追蹤航空器 位置，並得以控制獲得航空器上之視訊與數據資料。此自 動追蹤系統包括一航空器視訊傳送系統設於航空器上，一 地面自動追蹤航空器視訊系統，以及一地面控制站系統。 航空器視訊傳送系統包括一全球定位單元，一高度定位單 元，一攝影單元，一視訊資料下傳單元，一雙向語音數據 通訊單元，以及一微電腦處理單元。自動追蹤航空器視訊 系統，用以接收上述視訊與數據資料下傳單元與雙向語音 數據通訊單元下傳的資料，自動並傳送給控制站系統。當 4 本紙張尺度適用中國國家標準（CNS)/U規格（21〇 X 297公爱） -----------€------- 丨訂-------ί«^β^. (請先閱讀背面之注意事項再填寫本頁) 521153 8444twf.doc/009 Λ7 B7 五、發明說明（¾ ) 地面控制站系統依狀況需要，可透過追蹤航空器視訊系 統，控制航空器視訊傳送系統之攝影單元，取得視訊資料。 爲讓本發明之上述目的、特徵、和優點能更明顯易懂， 下文特舉一較佳實施例，並配合所附圖式，作詳細說明如 下： 圖式之簡單說明： 第1圖繪示依據本發明 動追蹤系統的架構； 第2圖繪示依據本發明 方塊圖； 第3圖繪示依據本發明 統之功能方塊圖；以及 第4圖繪示依據本發明 航空器視訊數據即時傳送自 航空器視訊傳送系統之功能 地面自動追蹤航空器視訊系 地面控制站系統之功能方塊 (請先閱讀背面之注意事項再填寫本頁) 圖 經濟部智慧財產局員工消費合作社印製 Λ 標號說明 100 102 104 106 108 110 112 114 116 航空器視訊傳送系統 微電腦處理器 攝影機 差分修正副載波接收單元 GPS或GLONASS雙頻接收單元 視訊監視單元 微波發射單元 衛星或GSM聲音數據通訊器 _星視訊發射與接收單元 -·1111111 « — — — — — — I— 本紙張尺度適用中國國家標準(CNS)A.l規恪（2ι〇χ 297公爱） 521153 8 4 4 4 twf. doc/0 0 9 Λ7 B7 五、發明說明d) 經濟部智慧財產局員工消費合作社印製 118 衛星聲音數據通訊單元 200 自動追蹤航空器視訊系統 202 微電腦自動追蹤伺服控制器 204 衛星、GSM聲音數據通訊器 206 微波接收器 208 微波追蹤天線 212 自動追蹤模式選控器 214 機械伺服控制器與機構 216 視訊監視器 218 衛星通訊視訊數據雙工天線 300 控制站系統 302 電腦系統 304 視訊監視器 306 航空器飛行路徑監視紀錄器 310 視訊遠端傳送器 312 視訊遠端接收器 314 衛星、GSM聲音通訊器 316 航空器網路全域追蹤定位器 318 衛星、GSM數據傳送系統 320 衛星數據資料傳送系統 322 衛星收發單元（視訊） 324 實施例 衛星聲音視訊通訊器 本發明提供一種航空器視訊數據即時傳送自動追蹤系 (請先閱讀背面之注意事項再填寫本頁) 本紙張尺度適用中國國家標準（CNS)A.丨規格（210 X 297公釐） 521153 84 44twf. doc/00 9 Λ7 B7 經濟部智慧財產局員工消費合作社印製 ^ 五、發明說明（b ) 統，得以雙向自動追蹤一飛行之航空器，以自動獲得視訊 (audio/video A/V)與數據資料，可包括影像，聲音，航空 器三維位置數據等相關的資料。然而數據資料可包括其他 的形式的資料。控制中心可主動選擇航空器的攝影裝置， 主動取得視訊資料，以得知攝影裝置所對應的監控處之狀 況’其可包括航空器內部的實況或是外部的實況^例如攝 影的地面狀況。本發明於航空器鹚地面控制之間，亘有控 制信號上傳㈣與視訊與_信號下傳= 功能。 本發明的航空器麵數據即時傳送自動追縱系統基本 上包括三個次系統。第1圖繪示依據本發明，航空器視訊 數據即時傳送自動追蹤系統的架_ 」木憐，其包括一航空器視訊 與數據傳送系統100，一自動追；Τ兄W 里刀坦嘥航空器視訊系統 以及一控制站系統300。此本鈐咖 匕小發日月系統可用於由一地面進 行對一航空器之即時追蹤，包括凹進 動偵測，也可即時攝取得影音薈如^ 〜曰 曰貪枓等。又可由地面控制站 系統3〇〇發出的攝影控制信號，路乱〜 ^啓動所欲之攝影裝置，以 監控選定處的實況。 於第1圖中，航空器視訊傳兔^… W得奂系統100架設於一航空 器上，用以偵測得到一視訊數 、数礙輿料包括一三維位置，一 語音，與一影像之複數個資料。 , ^ 努外且可將視訊數據資料 下傳，並可接收由控制方傳送中队i @出的一攝影控制信號，動態 控制攝取所欲之視訊數據資料。 ，地面自動追蹤航空器 ^命峴訊系統200，例如設置 另外 (請先閱讀背面之注意事項再填寫本頁)Because the current wireless communication technology is highly developed, it is also compatible with another global positioning system (GPS) or GLONASS positioning technology. If GPS, GLONASS dual-frequency sensing elements are set on the aircraft, the position of the aircraft corresponding to the ground can be accurately and automatically detected and transmitted to the ground control center. However, for the entire operating system, there is no complete aircraft tracking system. In addition, the current equipment design of the aircraft cannot transmit video data to the ground control center in real time, and currently only transmits voice data. Special 3 This paper size is in accordance with Chinese National Standard (CNS) A4 (210 x 297 mm) Printed by the Consumer Cooperatives of the Intellectual Property Bureau of the Ministry of Economic Affairs 521153 A7 8 4 44twf. Doc / 009 5. Description of the invention (V) The ground control center cannot directly control the aircraft and obtain video information. Especially when an emergency situation or hijack occurs on the aircraft, the ground control center cannot actively control the video equipment on the aircraft to grasp the actual condition on the aircraft. At present, in the traditional technology, there is still no complete and effective automatic tracking system for aircraft tracking and condition safety monitoring, which can effectively detect and track the path of the aircraft and the conditions that occur on site. In view of this, the present invention provides an automatic tracking system for real-time transmission of aircraft video data, which can immediately transmit video and audio data to a ground center for disasters. In addition, it can also be used for environmental protection, transportation, coastal patrol, etc., and immediately transfer audiovisual data to the ground center. It can also be applied to the battlefield conditions of the three-dimensional warfare of the National Army. It is activated when an emergency situation occurs in the cabin of a commercial airliner or during a hijacking. It can also take high-altitude photos. It is also beneficial to cooperate with the ground control center to establish an automatic tracking aircraft system. The invention provides an automatic tracking system for real-time transmission of aircraft video data, which can track the aircraft position by uploading and downloading video and data data, and can control the acquisition of video and data data on the aircraft. The automatic tracking system includes an aircraft video transmission system installed on the aircraft, a ground automatic tracking aircraft video system, and a ground control station system. The aircraft video transmission system includes a global positioning unit, an altitude positioning unit, a photographing unit, a video data transmission unit, a two-way voice data communication unit, and a microcomputer processing unit. The automatic tracking aircraft video system is used to receive the data transmitted by the video and data data downloading unit and the two-way voice data communication unit, and automatically transmit the data to the control station system. When 4 paper sizes are applicable to China National Standard (CNS) / U specifications (21〇X 297 public love) ----------- € ------- 丨 order ------ -ί «^ β ^. (Please read the notes on the back before filling this page) 521153 8444twf.doc / 009 Λ7 B7 V. Description of the invention (¾) The ground control station system can be tracked through the aircraft video system, Control the camera unit of the aircraft video transmission system to obtain video data. In order to make the above-mentioned objects, features, and advantages of the present invention more comprehensible, a preferred embodiment is given below in conjunction with the accompanying drawings for detailed description as follows: Brief description of the drawings: FIG. 1 shows The architecture of a motion tracking system according to the present invention; FIG. 2 shows a block diagram according to the present invention; FIG. 3 shows a functional block diagram according to the system of the present invention; and FIG. 4 shows real-time transmission of aircraft video data from the aircraft according to the present invention The function of the video transmission system The automatic ground tracking aircraft is the functional block of the ground control station system (please read the precautions on the back before filling this page). Figure Printed by the Intellectual Property Bureau Employee Consumer Cooperative of the Ministry of Economy 100 102 104 106 108 110 112 114 116 Aircraft video transmission system Microcomputer processor Camera differential correction sub-carrier receiving unit GPS or GLONASS dual frequency receiving unit Video monitoring unit Microwave transmitting unit Satellite or GSM sound data communicator_Star video transmitting and receiving unit- · 1111111 «— — — — — — I— This paper size applies Chinese National Standard (CNS) Al regulations 2ιχχ 297 public love) 521153 8 4 4 4 twf. Doc / 0 0 9 Λ7 B7 V. Description of the invention d) Printed by the Intellectual Property Bureau Staff Consumer Cooperative of the Ministry of Economy 118 Satellite sound data communication unit 200 Automatic tracking aircraft video system 202 Microcomputer automatic tracking servo controller 204 Satellite, GSM voice data communicator 206 Microwave receiver 208 Microwave tracking antenna 212 Automatic tracking mode selector 214 Mechanical servo controller and mechanism 216 Video monitor 218 Satellite communication video data duplex antenna 300 Control Station system 302 Computer system 304 Video monitor 306 Aircraft flight path monitoring recorder 310 Video remote transmitter 312 Video remote receiver 314 Satellite, GSM voice communicator 316 Aircraft network global tracking locator 318 Satellite, GSM data transmission system 320 satellite data and data transmission system 322 satellite transceiver unit (video) 324 embodiment satellite sound video communicator The present invention provides an automatic tracking system for real-time transmission of aircraft video data (please read the precautions on the back before filling this page) This paper size applies China Standard (CNS) A. 丨 Specifications (210 X 297 mm) 521153 84 44twf.doc / 00 9 Λ7 B7 Printed by the Consumers ’Cooperative of the Intellectual Property Bureau of the Ministry of Economic Affairs ^ V. Description of the invention (b) system, two-way automatic tracking Aircraft in flight to automatically obtain video (audio / video A / V) and data, which can include video, sound, and three-dimensional position data of the aircraft. However, the data may include other forms of information. The control center may actively select the camera device of the aircraft and actively obtain video data to learn the status of the monitoring location corresponding to the camera device. It may include the internal conditions of the aircraft or the external conditions ^ such as the ground conditions of the camera. The invention has functions of uploading control signals, video and _signal transmission = between aircraft and ground control. The automatic tracking system for instant transmission of aircraft surface data of the present invention basically includes three secondary systems. FIG. 1 shows a frame of an automatic tracking system for real-time transmission of aircraft video data in accordance with the present invention. The wooden frame includes an aircraft video and data transmission system 100 and an automatic tracking system. A control station system 300. This 钤 Ca 小 Xiaofa Sun and Moon system can be used for real-time tracking of an aircraft from a ground, including recessed motion detection, and can also capture video and audio such as ^ ~~ The camera control signal from the ground control station system 300 can be used to control the actual situation of the selected location. In the first figure, the aircraft video transmission rabbit ^ ... The W 100 system is installed on an aircraft to detect a video number, a number of obstacles including a three-dimensional position, a voice, and a plurality of images. data. , ^ It can download video data, and can receive a video control signal from the squadron i @ transmitted by the controller to dynamically control the acquisition of the desired video data. , Ground automatic tracking aircraft ^ Lifexon system 200, such as settings In addition (Please read the precautions on the back before filling this page)
· ϋ ϋ I n ϋ I ϋ I ϋ ϋ -I ϋ ϋ .1 ϋ J 本紙張尺度適用中國國家標準（CNS)Al規格 521153 Λ7· Ϋ ϋ I n ϋ I ϋ I ϋ ϋ -I ϋ ϋ .1 ϋ J This paper size applies to Chinese National Standard (CNS) Al specifications 521153 Λ7
8444twf.doc/009 五、發明說明（b ) 於地面之一基地（未示於圖），用以接收下傳之視訊數據裔 料，且利用天線裝置自動追蹤航空器之三維位置。並可傳 送出該視訊與數據資料及可能的相關資料。 地面控制站系統300,例如設置於地面之一控制中心， 接收地面自動追蹤航空器視訊系統傳送之相關^料，並且 可以發送該攝影控制信號，透過該地面自動追蹤航空器視 訊系統，以動態控制該航空器視訊傳送系統取得所欲之該 視訊數據資料。 上述之自動追蹤航空器視訊系統200與控制站系統 300，依實際運作，皆可設置於一可動之行動工具上^例 如可整合成一可動之系統，設置於可行動的車，船，或一 任務航空器上。 以下針對上述本發明的特徵，其三個次系統10〇,2〇〇， 300做進一步說明。 第2圖繪示依據本發明，航空器視訊傳送系統之功能 方塊圖，例如包括一微電腦處理器102，一攝影裝置104， 一差分（differential)修正副載波接收單元1〇6，一全球定位 系統GPS或GLONASS雙頻接收單元108，一視訊監視單 兀110，一微波發射單元112，一衛星或GSM聲音數據通 訊器114, 一衛星視訊發射與接收單元116,以及一衛星 聲音數據通訊單元118。 微電腦處理器102與其他周邊元件單元連接，用以處 理分析輸入數據，並且控制相關的周邊元件，進行自動追 蹤。攝影裝置104將取得的影像資料輸入給微電腦處理器 8 g張尺度適用中Θ國家標準（CNS)A·〗規格（210 X 297公釐) " "" --- ----!丨丨丨丨丨丨i丨丨丨丨—丨訂— (請先閱讀背面之注意事項再填寫本頁) , 經濟部智慧財產局員工消費合作社印絜 521153 A7 B7 84 4 4twf. doc/009 五、發明說明（η ) (請先閱讀背面之注意事項再填寫本頁) 102。攝影裝置104除了提供影像資訊外也可提供聲音資 訊。而就一般僅是影像的攝影時，其可例如包括紅外線攝 影機，彩色攝影機，黑白攝影機，或是星光攝影機等。攝 影機可包括至少一個，可設置於機艙內的一預定之處，也 可設置於機艙內的一處，以攝取航空器之外表面，或是地 面上之地形地物。攝影機的數量，及其監控的位置，可依 實際設計而變化。 差分修正副載波接收單元106,包括接收機部分與接 收天線部分。航空器在飛行時，除了器對應地面有一經緯 位置，也有一飛行高度。飛行高度之數據也是一種重要資 訊，特別是當地行起伏複雜時，高度是一重要參數。差分 修正副載波接收單元106可準確的測出航空器的高度，其 高度誤差可達到小於5公尺。而其對經緯度也具有明顯 修正效果。差分修正副載波接收單元106主要是利用差分 定位系統的技術Differential GPS (DGPS)達成。由地面基 地發射一參考信號，進行差分分析，以得知精確高度。 '經濟部智慧財產局員工消費合作社印製 全球定位系統GPS、GLONASS雙頻接收單元1〇8 ,可 感測出航空器的經緯地面位置，並將數據資料輸出給微電 腦處理器102。 視訊監視單元110由微電腦處理器102控制，用以航 空器上之任何監控。 微波發射單元112由微電腦處理器102控制，用以將 測得的任何資料，包括視訊數據資料等下傳給地面自動追 蹤航空器視訊系統200。 9 本紙張尺度適用中國國家標準（CNS)Α丨規格（21〇 X 297公餐） 521153 8 4 4 4twf. doc/0 0 9 A7 r---------Β7 五、發明說明（2 ) 衛星與行動通訊全球系統（global system f0r mobUe teleeommumcation，GSM)聲音數據通訊器114，與微電腦 處理器102雙向連接，用以與地面雙向通訊，並可藉由此 接受由地面發出之一攝影控制信號，以啓動選定的攝影機 1〇4，將視訊數據資料下傳或以客戶指定頻道控制之。 衛星視訊發射與接收單元116，以及一衛星聲音數據 通$單元118又提供另一管道與地面之控制中心雙向聯 絡，傳遞視訊數據或語音數據資料。 上述航空器視訊傳送系統可裝設於航空器的適當位 置’然而爲了易於將裝設此系統於航空器上而不影響到航 空器的安全，例如可將航空器視訊傳送系統的大部分裝備 裝設於飛機的莢艙(Pod)或與電子控制設備一倂裝設。 接著，第3圖繪示依據本發明，地面自動追蹤航空器 視訊系統之功能方塊圖。於第3圖中，地面自動追蹤航空 器視訊系統200包括一微電腦自動追蹤伺服控制器2〇2， 一衛星、GSM聲音數據通訊器204，一微波接收器206， 一微波追蹤天線208，一自動追蹤模式選控器212，一機 械伺服控制器與機構214，一視訊監視器216，以及一衛 星通訊視訊數據雙工天線218。 微電腦自動追蹤伺服控制器202，與其他周邊元件單 元連接，用以處理分析輸入數據，並且控制相關的周邊元 件。又微電腦自動追蹤伺服控制器202可與地面控制站系 統3 00進行數據資料相互傳輸，其也可包括其他相關杳料 的傳輸。 本纸張尺度適用中國國家標準（CNS)A4規格（210 X 297公餐） (請先閱讀背面之注意事項再填寫本頁) .Μψ--------tr--------- ，經濟部智慧財產局員工消費合作社印製 521153 Λ7 B7 8444twf.doc/009 五、發明說明（q ) 由於本發明系統能追蹤航空器位置，衛星、GSM聲 音數據通訊器204，可與航空器視訊傳送系統1〇〇進行雙 向通訊。另外，當例如航空器發生緊急狀況，又例如劫機 事件發生，可由微電腦自動追蹤伺服控制器202，發出攝 影控制信號給航空器視訊傳送系統100，以選擇啓動其上 之攝影機104進行了解實況。當航空器因任務需要，可啓 動相關的攝影機104，進行實況紀錄。 微波接收器206與微波追蹤天線208構成一追蹤單 元。微波接收器206將下傳的視訊數據資料，分解出影像， 聲音’與DGPS資料，並輸入給微電腦自動追蹤伺服控制 器202。進而根據航空器位置，控制機械伺服控制器與機 構21。微波追蹤天線208可由機械伺服控制器與機構214 控制’使其對準追蹤航空器。由於本發明系統能追蹤航空 器位置’因此也藉由對準的天線系統208，進行雙向通訊， 例如又包括一衛星通訊視訊數據雙工天線218。 追蹤選擇控制器212，可用以選定一追蹤模式，其包 括一手動追蹤模式與自動追蹤模式。依實際需要，可選擇 其中一追蹤模式，即時自動追蹤航空器。另外視訊監視器 216可做爲一般安全監控。 當地面自動追蹤航空器視訊系統200接收到下傳的視 訊數據資料時，也會同時將視訊數據資料傳送到地面控制 中心。此中心設置有一地面控制站系統3〇〇。第4圖繪示 依據本發明，地面控制站系統之功能方塊圖。地面控制站 系統包括一電腦系統302，一視訊監視及錄影裝置3〇4， 本纸張尺度適用中國國家標準（CNS)A丨規烙（21〇χ 297公餐） n I ϋ ϋ ϋ em§ ί ί n n · a— amt ϋ n emm§ i -n · 1· an ϋ Hi ϋ Marne ai I (請先閱讀背面之注意事項再填寫本頁) •經濟部智慧財產局員工消費合作社印製 521153 Λ7 B7 8 444twf. doc/009 五、發明說明（1° ) (請先閱讀背面之注意事項再填寫本頁) 一航空器飛行路徑監視記錄器306，一視訊遠端傳送器 310，一衛星、GSM聲音通訊器314，以及一航空器網路 全域追蹤定位器316，GSM數據傳送系統318，衛星數據 資料傳送系統320，衛星收發單元（視訊）322，以及衛星聲 音視訊通訊器324。 電腦系統302，與上述其他周邊單元連接，同時接收 微電腦自動追蹤伺服控制器202 (見第3圖）或衛星，所傳 來的所有視訊資料，並進行周邊單元的必要控制與處理動 作。 視訊監視及錄影裝置304，連接至電腦系統3〇2做爲 一般監視與錄影。 航空器飛行路徑監視記錄器306,以記錄航空器之飛 行路徑。 對外通訊單元，例如視訊遠端傳送器310，其可傳送 視訊資料給一視訊遠端接收器312,與一遠端使用者進行 通訊與資料傳輸。 聲音通訊單元，包括衛星、GSM聲音通訊器314，可 藉由衛星、GSM系統與其他使用者進行通訊與資料傳輸。 '經濟部智慧財產局員工消費合作社印製 航空器網路全域追蹤定位器316,提供另一通訊路徑， 可透過網路，與相關者進行通訊與資料傳輸。然而若是視 訊無法成功被接收到，其可又透過GSM數據系統318，或 是另一衛星數據資料傳送系統320將數據資料進一步傳遞 出去。 又，電腦系統302也與衛星收發單元（視訊）322以及 12 本紙張尺度適用中國國家標準（CNS)Al規格（210 X 297公餐） 521153 A7 B7 8444twf.doc/009 五、發明說明（u ) 衛星聲音視訊通訊器324連接，可透過衛星系統進行視訊 或語音數據的雙向傳輸。 本發明已建立完整之微波視訊，聲音，數位資訊等射 接收系統之設計。使地面可有效追蹤航空器之飛行狀況。 本發明在航空器上，特別包括差分（differential)修正 副載波接收單元106,如此得以準確測得知航空器經緯度 高度，並且傳送給地面。 本發明在航空器上，又例如使用GSM、GLONASS通 訊系統，使地面能上傳控制信號，以選擇器動航空器上的 攝影系統，向地面自動下傳視訊據資料。 本發明由於能追蹤航空器，因此也可藉由天線系統對 準航空器，上傳（up-link)資料，也因此例如能控制航空器 上的攝影系統，例如在狀況發生時可直接主動監視航空器 上的狀況。 本發明上述之自動追縱航空器視訊系統200與控制站 系統300，依實際運作，皆可設置於一可動之行動工具上， 例如可整合成一可動之系統，設置於可行動的車，船，或 一任務航空器上。 本發明在整體系統而言，使得航空器與地面之間，得 以雙向傳輸資料與信號，達成自動追蹤的目的。 本發明之航空器追蹤系統，例如可適用於： 1·災害，例如地震，火災，水災，救難等之即時影 音數據資料下傳。 2.環保，交通，海岸巡防等之即時將影音數據資料 13 本紙張尺度適用中國國家標準（CNS)A4規格（210 X 297公釐） (請先閱讀背面之注意事項再填寫本頁) t ·— an· a·· 9 μμ μ·· βην I 篇 m '經濟部智慧財產局員工消費合作社印製 521153 8444twf.d〇c/〇〇9 五、發明說明 下傳。 3·軍事立體作戰時之戰場狀況，即時將影音數據資 料下傳。 4·簡用客機機艙，例如發生緊急狀況或劫機時，可 啓動選定攝影機，即時將影音數據資料下傳。 5·阓空空照，例如演習，災區，即時將影音數據資 料下傳。 6·新聞報導，例如電視台新聞快報，即時將影音數 據資料下傳。 7·又可配合地面控制中心，建立自動追蹤航空器的 系統’其又可應用於雷達自動追蹤，自動化武器射擊裝備， 高倍率重載型攝影機，或船舶、車輛行進中之衛星天線自 動追蹤系統接收即時衛星節目。 綜上所述，雖然本發明已以一較佳實施例揭露如上， 然其並非用以限定本發明，任何熟習此技藝者，在不脫離 本發明之精神和範圍內，當可作各種之更動與潤飾，因此 本發明之保護範圍當視後附之申請專利範圍所界定者爲 準。 ----------i — — — — — — — — — — — — <請先閱讀背面之注意事項再填寫本頁) •經濟部智慧財產局員工消費合作社印製 14 本紙張尺度適用中國國家標準（CNS)A·丨規格（210 X 297公釐]8444twf.doc / 009 V. Description of the invention (b) A base on the ground (not shown in the figure), used to receive the video data and download the data, and use the antenna device to automatically track the three-dimensional position of the aircraft. And can send the video and data materials and possibly related information. The ground control station system 300, for example, is located in a control center on the ground, receives relevant materials transmitted by the ground automatic tracking aircraft video system, and can send the photographic control signal through the ground automatic tracking aircraft video system to dynamically control the aircraft. The video transmission system obtains the desired video data. The above-mentioned automatic tracking aircraft videoconferencing system 200 and control station system 300 can be installed on a movable mobile tool according to actual operation. For example, it can be integrated into a movable system and installed on a movable vehicle, ship, or a mission aircraft. on. The three sub-systems 100, 200, and 300 of the above-mentioned features of the present invention are further described below. FIG. 2 shows a functional block diagram of an aircraft video transmission system according to the present invention, including, for example, a microcomputer processor 102, a photographing device 104, a differential modified subcarrier receiving unit 106, and a global positioning system GPS Or GLONASS dual-frequency receiving unit 108, a video surveillance unit 110, a microwave transmitting unit 112, a satellite or GSM sound data communicator 114, a satellite video transmitting and receiving unit 116, and a satellite sound data communication unit 118. The microcomputer processor 102 is connected to other peripheral component units to process and analyze input data, and controls related peripheral components for automatic tracking. The photographing device 104 inputs the acquired image data to the microcomputer processor 8 g-size standard applicable Θ National Standard (CNS) A ·〗 Specifications (210 X 297 mm) " " " --- ----!丨 丨 丨 丨 丨 丨 i 丨 丨 丨 丨 ——— Order— (Please read the precautions on the back before filling this page), the Intellectual Property Bureau Employee Consumer Cooperatives of the Ministry of Economic Affairs seal 521153 A7 B7 84 4 4twf. Doc / 009 5 2. Description of the invention (η) (Please read the notes on the back before filling in this page) 102. The camera 104 can provide audio information in addition to image information. In general, when the image is only taken, it may include, for example, an infrared camera, a color camera, a black and white camera, or a starlight camera. The camera may include at least one, which may be arranged at a predetermined place in the cabin, or may be arranged at a place in the cabin to capture the external surface of the aircraft or the terrain features on the ground. The number of cameras and the locations they monitor can vary depending on the actual design. The differentially modified subcarrier receiving unit 106 includes a receiver portion and a receiving antenna portion. When the aircraft is flying, in addition to the latitude and longitude position corresponding to the ground, the aircraft also has a flying altitude. Flight altitude data is also an important piece of information, especially when the local travel is undulating and complex, altitude is an important parameter. The differentially-corrected subcarrier receiving unit 106 can accurately measure the altitude of an aircraft, and its height error can reach less than 5 meters. And it has obvious correction effect on latitude and longitude. The differential correction subcarrier receiving unit 106 is mainly achieved by using a differential positioning system technology, Differential GPS (DGPS). A reference signal is transmitted from the ground base and a differential analysis is performed to obtain the precise altitude. 'The Intellectual Property Bureau of the Ministry of Economic Affairs ’employee consumer cooperative printed a global positioning system GPS and GLONASS dual-frequency receiving unit 108, which can sense the longitude and latitude ground position of the aircraft and output the data to the microcomputer processor 102. The video surveillance unit 110 is controlled by the microcomputer processor 102 for any monitoring on the aircraft. The microwave transmitting unit 112 is controlled by the microcomputer processor 102, and is used to transmit any measured data, including video data, to the ground automatic tracking aircraft video system 200. 9 This paper size applies Chinese National Standard (CNS) A 丨 specifications (21〇X 297 meals) 521153 8 4 4 4twf. Doc / 0 0 9 A7 r --------- B7 V. Description of the invention ( 2) Global system f0r mobUe teleeommumcation (GSM) voice data communicator 114 is bidirectionally connected to the microcomputer processor 102 for two-way communication with the ground, and can accept a photo sent from the ground through this Control signal to start the selected camera 104, download the video data or control it with the channel specified by the customer. The satellite video transmitting and receiving unit 116, and a satellite sound data communication unit 118 provide another channel for two-way communication with the ground control center to transfer video data or voice data. The above-mentioned aircraft video transmission system can be installed in an appropriate position of the aircraft. However, in order to easily install the system on the aircraft without affecting the safety of the aircraft, for example, most of the equipment of the aircraft video transmission system can be installed in the pod of the aircraft. Pod or installed with electronic control equipment. Next, FIG. 3 shows a functional block diagram of a ground automatic tracking aircraft video system according to the present invention. In FIG. 3, the ground automatic tracking aircraft video system 200 includes a microcomputer automatic tracking servo controller 202, a satellite, GSM voice data communicator 204, a microwave receiver 206, a microwave tracking antenna 208, and an automatic tracking The mode selector 212, a mechanical servo controller and mechanism 214, a video monitor 216, and a satellite communication video data duplex antenna 218. The microcomputer automatically tracks the servo controller 202 and is connected to other peripheral component units to process and analyze input data and control related peripheral components. In addition, the microcomputer automatic tracking servo controller 202 can perform data transmission with the ground control station system 300, and it can also include transmission of other related materials. This paper size is applicable to China National Standard (CNS) A4 specification (210 X 297 meals) (Please read the precautions on the back before filling this page) .Μψ -------- tr ------ --- ， Printed by the Consumer Cooperative of the Intellectual Property Bureau of the Ministry of Economic Affairs 521153 Λ7 B7 8444twf.doc / 009 V. Description of the invention (q) Because the system of the present invention can track the position of the aircraft, the satellite and GSM voice data communicator 204 can be used with the aircraft The video transmission system 100 performs two-way communication. In addition, when, for example, an emergency situation occurs in the aircraft and a hijacking event occurs, the microcomputer can automatically track the servo controller 202 to send a camera control signal to the aircraft video transmission system 100 to select the camera 104 to be activated to learn the actual situation. When the aircraft requires it, the relevant camera 104 can be activated for live recording. The microwave receiver 206 and the microwave tracking antenna 208 constitute a tracking unit. The microwave receiver 206 decomposes the downloaded video data data into video, sound 'and DGPS data, and inputs them to the microcomputer automatic tracking servo controller 202. Based on the aircraft position, the mechanical servo controller and mechanism 21 are controlled. The microwave tracking antenna 208 may be controlled ' by the mechanical servo controller and mechanism 214 to align it with the tracking aircraft. Since the system of the present invention can track the position of the aircraft ', it also uses the aligned antenna system 208 for two-way communication, for example, it also includes a satellite communication video data duplex antenna 218. The tracking selection controller 212 can be used to select a tracking mode, which includes a manual tracking mode and an automatic tracking mode. According to actual needs, one of the tracking modes can be selected to automatically track the aircraft in real time. In addition, the video monitor 216 can be used for general security monitoring. When the ground automatic tracking aircraft video system 200 receives the downloaded video data, it will also transmit the video data to the ground control center at the same time. This center is equipped with a ground control station system 300. Figure 4 shows a functional block diagram of the ground control station system according to the present invention. The ground control station system includes a computer system 302, a video surveillance and video recording device 304. This paper standard is applicable to China National Standard (CNS) A 丨 Regulation (21〇χ 297 meals) n I ϋ ϋ ϋ em§ ί ί nn · a— amt ϋ n emm§ i -n · 1 · an ϋ Hi ϋ Marne ai I (Please read the precautions on the back before filling out this page) • Printed by the Intellectual Property Bureau Employee Consumer Cooperative of the Ministry of Economic Affairs 521153 Λ7 B7 8 444twf. Doc / 009 V. Description of the invention (1 °) (Please read the notes on the back before filling this page) An aircraft flight path monitoring recorder 306, a video remote transmitter 310, a satellite, GSM sound Communicator 314, and an aircraft network global tracking locator 316, GSM data transmission system 318, satellite data transmission system 320, satellite transceiver unit (video) 322, and satellite sound video communicator 324. The computer system 302 is connected with the other peripheral units mentioned above, and simultaneously receives all video data from the microcomputer automatic tracking servo controller 202 (see Fig. 3) or satellite, and performs necessary control and processing operations of the peripheral units. The video surveillance and recording device 304 is connected to the computer system 302 for general surveillance and recording. The aircraft flight path monitoring recorder 306 records the flight path of the aircraft. An external communication unit, such as a video remote transmitter 310, can transmit video data to a video remote receiver 312 for communication and data transmission with a remote user. The sound communication unit, including satellite and GSM sound communicator 314, can communicate and transmit data with other users through satellite and GSM system. 'Printed by the Consumer Cooperative of the Intellectual Property Bureau of the Ministry of Economic Affairs, the aircraft network global tracking locator 316 provides another communication path, which can be used for communication and data transmission with relevant parties through the network. However, if the video cannot be successfully received, it can be further transmitted through the GSM data system 318 or another satellite data transmission system 320. In addition, the computer system 302 and the satellite transceiver unit (video) 322 and 12 paper standards are applicable to the Chinese National Standard (CNS) Al specification (210 X 297 meals) 521153 A7 B7 8444twf.doc / 009 V. Description of the invention (u) The satellite sound video communicator 324 is connected, and can perform two-way transmission of video or voice data through a satellite system. The invention has established a complete microwave video, audio, digital information and other radio receiving system design. The ground can effectively track the flight conditions of the aircraft. The invention specifically includes a differential correction subcarrier receiving unit 106 on the aircraft, so that the aircraft's latitude, longitude and altitude can be accurately measured and transmitted to the ground. On the aircraft, the invention also uses GSM and GLONASS communication systems to enable the ground to upload control signals to select a camera system on the aircraft to automatically transmit video data to the ground. Because the invention can track the aircraft, it can also use the antenna system to aim the aircraft and upload (up-link) data. Therefore, for example, the camera system on the aircraft can be controlled. For example, when the situation occurs, it can directly monitor the situation on the aircraft. . According to the actual operation, the automatic tracking aircraft videoconferencing system 200 and the control station system 300 of the present invention can be installed on a movable mobile tool, for example, can be integrated into a movable system and installed on a movable vehicle, ship, or On a mission aircraft. In terms of the overall system, the present invention enables two-way transmission of data and signals between the aircraft and the ground to achieve the purpose of automatic tracking. The aircraft tracking system of the present invention can be applied, for example, to: 1. Dispatching real-time audiovisual data of disasters, such as earthquakes, fires, floods, rescues, etc. 2. Environmental protection, transportation, coastal patrols, etc. will immediately include audio and video data. 13 This paper size applies to China National Standard (CNS) A4 (210 X 297 mm) (please read the precautions on the back before filling this page) t · — An · a ·· 9 μμ μ ·· βην I Article m 'Printed by the Consumer Consumption Cooperative of the Intellectual Property Bureau of the Ministry of Economy 521153 8444twf.d〇c / 〇〇9 5. The description of the invention will be transmitted. 3. The battlefield conditions during the three-dimensional military operations, the video and audio data will be transmitted immediately. 4. Simply use the cabin of the passenger plane. For example, in the event of an emergency or hijacking, you can activate the selected camera to download the audio and video data in real time. 5. Take aerial photos, such as drills, disaster areas, and immediately transfer audiovisual data. 6. News reports, such as the news bulletin of the TV station, download the audiovisual data in real time. 7. It can also cooperate with the ground control center to establish an automatic tracking aircraft system. It can also be used for automatic radar tracking, automatic weapon shooting equipment, high magnification heavy-duty cameras, or satellite antenna automatic tracking systems during ship and vehicle travel. Instant satellite shows. In summary, although the present invention has been disclosed as above with a preferred embodiment, it is not intended to limit the present invention. Any person skilled in the art can make various changes without departing from the spirit and scope of the present invention. And retouching, so the scope of protection of the present invention shall be determined by the scope of the attached patent application. ---------- i — — — — — — — — — — — — < Please read the notes on the back before filling out this page) • 14 copies printed by the Intellectual Property Bureau Staff Consumer Cooperatives of the Ministry of Economic Affairs Paper size applies to China National Standard (CNS) A · 丨 specifications (210 X 297 mm)