TWM577993U - Advancing observation system of unmanned aerial vehicle - Google Patents
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Abstract
一種無人機之前進觀測系統,其係具有一無人機,該無人機係透過一偵測元件發現一目標物,並產生有一目標物參數,且該無人機透過一第一訊號收發元件以無線方式連接有一觀測平台之第二訊號收發元件,使該無人機之位置參數與該目標物參數資料傳輸至該觀測平台,再透過一計算元件分析計算目標物坐標位置,並將分析計算後的結果顯示於一顯示單元,以檢視目標物位置,藉此,透過該無人機先進行偵蒐情報,接著透過該觀測平台進行參數運算,且該無人機無地域限制特性,且可快速獲得目標位置,以確保人員安全提升觀測效能。An unmanned aerial vehicle front observation system, which has an unmanned aerial vehicle that discovers a target through a detecting component and generates a target parameter, and the drone is wirelessly transmitted through a first signal transmitting and receiving component Connecting a second signal transceiving component of the observation platform, the position parameter of the UAV and the target parameter data are transmitted to the observation platform, and then calculating a coordinate position of the target object through a calculation component, and displaying the result of the analysis and calculation The display unit is configured to view the position of the target object, thereby performing the search information through the unmanned aerial vehicle, and then performing parameter calculation through the observation platform, and the drone has no geographical limitation characteristic, and the target position can be quickly obtained. Ensure personnel safety and improve observation performance.
Description
本創作係與一種無人機有關,特別是指一種無人機之前進觀測系統。This creation is related to a drone, especially a drone advance observation system.
按,習知地面觀測方式,係透過人員前進敵陣地觀測攻擊目標,其會受限地形或危險區域的限制無法觀測,且會增加人員之危險,更降低目標的觀測效能,此外,地面觀測透過人員實測,故目標的位置座標會有誤差,進而降低觀測的效能,是以,本案創作人在觀察到上述缺點後,認為習知的觀測方式實有改進之必要,而遂有本創作之產生。According to the conventional ground observation method, the target is observed through the enemy's forward position, which is limited by the limited terrain or dangerous area, and increases the danger of the personnel and reduces the observation performance of the target. The personnel measured, so the position coordinates of the target will have errors, which will reduce the effectiveness of the observation. Therefore, after observing the above shortcomings, the creator of the case believes that the conventional observation method is necessary to improve, and the creation of this creation is not necessary. .
本創作之目的係在提供一種無人機之前進觀測系統,係透過無人機先執行情報偵蒐任務,以蒐集目標物參數資料,提升觀測效能之目的。The purpose of this creation is to provide an observation system before the drone, and to perform an intelligence investigation task through the drone to collect the target parameter data and improve the observation performance.
為達上述目的,本創作所提供之無人機之前進觀測系統,其係包含有:一無人機,其係具有一定位元件,該定位元件係產生有一無人機位置參數,且該無人機係透過至少一偵測元件,以產生有一目標物測量參數,又該無人機係包含有一第一訊號收發元件;以及一觀測平台,其係具有一顯示元件,且該顯示元件電性連接有一地圖資料庫,又該觀測平台係具有一第二訊號收發件,該第二訊號收發件與該第一訊號收發件係以無線方式相連接,使該第二訊號收發元件接收該無人機位置參數以及該目標物測量參數資料,並透過一計算元件進行分析計算目標物坐標位置,且該計算元件係電性連接該地圖資料庫,使分析計算後的結果顯示於該顯示元件。In order to achieve the above objective, the present invention provides a UAV forward observation system, which comprises: a UAV having a positioning component, the positioning component generates a UAV position parameter, and the UAV transmits At least one detecting component to generate a target measurement parameter, the UAV includes a first signal transceiving component; and an observation platform having a display component, and the display component is electrically connected to a map database And the observation platform has a second signal transceiver, the second signal transceiver is wirelessly connected to the first signal transceiver, and the second signal transceiver component receives the drone position parameter and the target The object measures the parameter data, and analyzes and calculates the coordinate position of the target object through a computing component, and the computing component is electrically connected to the map database, so that the analysis and calculation result is displayed on the display component.
本創作所提供之無人機之前進觀測系統,係透過該無人機係透過偵測元件發現一目標物,並產生該目標物測量參數,且透過該第一訊號收發元件以無線傳輸方式連接該第二訊號收發元件,使該無人機之位置參數與該目標物測量參數資料傳輸至該觀測平台,接著透過該計算元件進行分析計算該目標物坐標位置,且該計算元件係連接該地圖資料庫,並顯示於該顯示元件,以檢視該目標物位置,藉此,透過該無人機先進行偵蒐情報,接著透過該觀測平台進行參數運算,且該無人機無地域限制特性,且可快速獲得目標位置,以確保人員安全提升觀測效能。The drone forward observation system provided by the present invention detects an object through the detecting component through the unmanned aerial vehicle, generates the target measurement parameter, and connects the first wireless transmission and transmission component through the first signal transmitting and receiving component. a second signal transceiving component, wherein the position parameter of the UAV and the target measurement parameter data are transmitted to the observation platform, and then the target coordinate position is analyzed and calculated through the computing component, and the computing component is connected to the map database. And displaying the display component to view the target position, thereby performing the Detective Intelligence through the UAV, and then performing parameter calculation through the observation platform, and the UAV has no geographical limitation characteristics, and can quickly obtain the target. Location to ensure personnel safety and improve observation performance.
請參閱第1圖所示,係本創作之較佳實施例之系統方塊圖,其係揭露有一種無人機之前進觀測系統100,係包含有:Referring to FIG. 1, a system block diagram of a preferred embodiment of the present invention discloses a drone advance observation system 100, which includes:
一無人機10,其係具有一定位元件11,該定位元件11係為GPS,該定位元件11係產生有一無人機位置參數,又該無人機10係具有一第一偵測元件12以及一第二偵測元件13,該無人機10係透過該第一偵測元件12以及該第二偵測元件13發現一目標物,並產生有一目標物測量參數,該目標物測量參數係包含有方位角、距離以及俯仰角,於本實施例中,該第一偵測元件12係為UAV陀螺儀,而可取得目標物200之UAV方向角,該第二偵測元件13係為雷射測距儀,而可觀測目標物之距離,且透過該第一偵測元件12以及第二偵測元件13取得俯仰角,此外,該無人機10係具有一第一訊號收發元件14,且該第一訊號收發元件14、該定位元件11、該第一偵測元件12以及該第二偵測元件13係電性相連接,並透過該第一訊號收發元件14傳輸該無人機位置參數與該目標物測量參數。An unmanned aerial vehicle 10 having a positioning component 11 is a GPS, the positioning component 11 generates a UAV position parameter, and the UAV 10 has a first detecting component 12 and a first a detecting component 13 , the drone 10 discovering an object through the first detecting component 12 and the second detecting component 13 , and generating a target measurement parameter, where the target measurement parameter includes an azimuth In the present embodiment, the first detecting component 12 is a UAV gyroscope, and the UAV direction angle of the target object 200 is obtained, and the second detecting component 13 is a laser range finder. Observing the distance of the target object, and obtaining the pitch angle through the first detecting component 12 and the second detecting component 13 , wherein the drone 10 has a first signal transceiving component 14 and the first signal The transceiver component 14, the positioning component 11, the first detecting component 12, and the second detecting component 13 are electrically connected, and transmit the UAV position parameter and the target measurement through the first signal transceiving component 14. parameter.
一觀測平台20,其係具有一顯示元件21,該顯示元件21係為一螢幕,且該顯示元件21係電性相接有一地圖資料庫22,又該觀測平台20係具有一第二訊號收發元件23,該第二訊號收發元件23與該第一訊號收發元件14係以無線方式相連接,使該第二訊號收發元件23接收該無人機位置參數以及該目標物測量參數資料,並透過一計算元件24進行分析計算目標物坐標位置,且該計算元件24係電性連接該地圖資料庫22,使分析計算後的結果顯示於該顯示元件21,又該計算元件24係連接有一目標確認元件25,以確認該目標物,且該目標確認元件25係電性連接一命名元件26,該命名元件26係以命名該目標物的名稱。An observation platform 20 has a display component 21, the display component 21 is a screen, and the display component 21 is electrically connected to a map database 22, and the observation platform 20 has a second signal transmission and reception. The second signal transceiving component 23 is connected to the first signal transceiving component 14 in a wireless manner, so that the second signal transceiving component 23 receives the UAV position parameter and the target measurement parameter data, and transmits the The computing component 24 performs an analysis and calculation of the target coordinate position, and the computing component 24 is electrically connected to the map database 22, so that the analysis and calculation result is displayed on the display component 21, and the computing component 24 is connected to a target confirmation component. 25, to confirm the target, and the target confirmation component 25 is electrically connected to a named component 26, the named component 26 is named to name the target.
為供進一步瞭解本創作構造特徵、運用技術手段及所預期達成之功效,茲將本創作使用方式加以敘述,相信當可由此而對本創作有更深入且具體之瞭解,如下所述:In order to further understand the characteristics of this creation, the use of technical means and the expected results, we will describe the use of this creation, and believe that we can have a deeper and more specific understanding of this creation, as follows:
請參閱第1圖、第2圖以及第3圖所示,首先,該無人機10透過該第一偵測元件12以及該第二偵測元件13偵測目標物200,以獲得該目標物測量參數,並透過該第一訊號收發元件14以無線方式連接該第二訊號收發元件23,使該無人機位置參數與該目標物測量參數資料傳輸至該觀測平台20,接著透過該計算元件24進行該目標物測量參數演算,以分析計算該目標物200坐標位置,且該計算元件24係連接該地圖資料庫22,並顯示於該顯示元件21,如第4圖所示,再透過該目標確認元件25進行目標物確認,若當目標物確認正確時,透過該命名元件26進行目標物命名,並回傳至後方指揮中心,當目標物確認取消時,該無人機10則返回重新搜尋目標物,以獲得目標物測量參數,並對目標物參數演算,以重新確認該目標物200,藉此,透過該無人機10先進行偵蒐情報,接著透過該觀測平台20進行參數運算,且該無人機10無地域限制特性,快速獲得目標位置,以確保人員安全提升觀測效能。Referring to FIG. 1 , FIG. 2 and FIG. 3 , firstly, the drone 10 detects the target object 200 through the first detecting component 12 and the second detecting component 13 to obtain the target measurement. Parameter, and wirelessly connecting the second signal transceiving component 23 through the first signal transceiving component 14 to transmit the UAV position parameter and the target measurement parameter data to the observing platform 20, and then through the computing component 24 The target measurement parameter calculation is performed to analyze and calculate the coordinate position of the target object 200, and the computing component 24 is connected to the map database 22 and displayed on the display element 21, as shown in FIG. 4, and then confirmed by the target. The component 25 performs the object confirmation. If the target object is confirmed correctly, the target object is named by the name component 26 and is transmitted back to the rear command center. When the target object is confirmed to be canceled, the drone 10 returns to search for the target object again. Obtaining the target measurement parameter and calculating the target parameter to re-confirm the target 200, thereby performing the Detective Intelligence through the UAV 10, and then transmitting the observation 20-parameter calculation, and the UAV 10 properties without geographical restrictions, quick access to the target location, in order to ensure the safety of personnel to enhance the effectiveness of the observation.
值得一提的是,上述該第一偵測元件12係為UAV陀螺儀,使該第一偵測元件12取得UAV方位角,而該第二偵測元件13係為雷射測距設備,以雷射測距觀測目標,藉此,透過該第一偵測元件12以及該第二偵測元件13測得該目標物俯仰角測量參數,並透過該第一訊號收發元件14回傳至該觀測平台20,以進行目標坐標演算,並獲得目標坐標位置。It is worth mentioning that the first detecting component 12 is a UAV gyroscope, so that the first detecting component 12 obtains a UAV azimuth, and the second detecting component 13 is a laser ranging device. a target of the laser ranging observation, wherein the target pitch angle measurement parameter is measured by the first detecting component 12 and the second detecting component 13 and transmitted back to the observation through the first signal transceiving component 14 The platform 20 performs target coordinate calculation and obtains a target coordinate position.
值得再提的是,透過該觀測平台20確認目標物及命名目標物後,待命令透過電波獲光波及其他載體彼此連線,以回傳後方指揮中心。It is worth mentioning that after confirming the target object and naming the target object through the observation platform 20, it is required to transmit the light wave and other carriers through the electric wave to connect to each other to return the rear command center.
茲,再將本創作之特徵及其可達成之預期功效陳述如下:Hereby, the characteristics of this creation and its achievable expected effects are stated as follows:
本創作所提供之無人機之前進觀測系統,係透過該無人機10係透過該第一偵測元件以及該第二偵測元件發現該目標物200,並產生該目標物參數,且透過該第一訊號收發元件14以無線傳輸方式連接該第二訊號收發元件23,使該無人機之位置參數與該目標物測量參數資料傳輸至該觀測平台20,接著透過該計算元件24進行分析計算該目標物坐標位置,且該計算元件24係連接該地圖資料庫22,並顯示於該顯示元件21,藉此,透過該無人機10先進行偵蒐情報,接著透過該觀測平台20進行參數運算,且該無人機10無地域限制特性,快速獲得目標位置,以確保人員安全提升觀測效能。The drone advance observation system provided by the present invention detects the target object 200 through the first detecting component and the second detecting component through the drone 10, and generates the target parameter, and transmits the target parameter A signal transceiving component 14 is connected to the second signal transceiving component 23 by wireless transmission, and transmits the position parameter of the UAV and the target measurement parameter data to the observing platform 20, and then analyzes and calculates the target through the computing component 24. An object coordinate position, and the computing component 24 is connected to the map database 22 and displayed on the display component 21, whereby the unmanned aerial vehicle 10 first performs reconnaissance information, and then performs parameter calculation through the observation platform 20, and The UAV 10 has no geographically restricted features and quickly obtains a target location to ensure personnel safety and improve observation performance.
綜上所述,本創作在同類產品中實有其極佳之進步實用性,同時遍查國內外關於此類結構之技術資料,文獻中亦未發現有相同的構造存在在先,是以,本創作實已具備新型專利要件,爰依法提出申請。In summary, this creation has its excellent progress and practicality in similar products. At the same time, it has investigated the technical information about such structures at home and abroad. The same structure has not been found in the literature. This creation has already possessed new types of patent requirements, and applied for it according to law.
惟,以上所述者,僅係本創作之一較佳可行實施例而已,故舉凡應用本創作說明書及申請專利範圍所為之等效結構變化,理應包含在本創作之專利範圍內。However, the above-mentioned ones are only one of the preferred embodiments of the present invention, and the equivalent structural changes in the application of the present specification and the scope of the patent application are intended to be included in the scope of the present patent.
100‧‧‧無人機之前進觀測系統100‧‧‧Unmanned aerial vehicle forward observation system
10‧‧‧無人機 10‧‧‧ drones
11‧‧‧定位元件 11‧‧‧ Positioning components
12‧‧‧第一偵測元件 12‧‧‧First detection component
13‧‧‧第二偵測元件 13‧‧‧Second detection component
14‧‧‧第一訊號收發元件 14‧‧‧First signal transceiver component
20‧‧‧觀測平台 20‧‧‧ Observing platform
21‧‧‧顯示元件 21‧‧‧ Display elements
22‧‧‧地圖資料庫 22‧‧‧Map Database
23‧‧‧第二訊號收發元件 23‧‧‧Second signal transceiver component
24‧‧‧計算元件 24‧‧‧Computational components
25‧‧‧目標確認元件 25‧‧‧ Target confirmation component
26‧‧‧命名元件 26‧‧‧Named components
200‧‧‧目標物 200‧‧‧ Targets
第1圖係本創作之較佳實施例之系統方塊圖。 第2圖係本創作之較佳實施例之流程示意圖。 第3圖係本創作之較佳實施例之無人機偵測目標物示意圖。 第4圖係本創作之較佳實施例之觀測平台顯示無人機與目標物位置示意圖。Figure 1 is a block diagram of a system of a preferred embodiment of the present invention. Figure 2 is a schematic flow diagram of a preferred embodiment of the present invention. Figure 3 is a schematic diagram of the unmanned aerial vehicle detection target of the preferred embodiment of the present invention. Figure 4 is a schematic diagram showing the position of the drone and the target object by the observation platform of the preferred embodiment of the present invention.
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TWI762924B (en) * | 2019-09-11 | 2022-05-01 | 美商惠普發展公司有限責任合夥企業 | Measurement devices |
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