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TW201709000A - Escort service management method and system for unmanned aerial vehicle providing automatic escort of unmanned aerial vehicle to reach a vacant stay-in site - Google Patents

Escort service management method and system for unmanned aerial vehicle providing automatic escort of unmanned aerial vehicle to reach a vacant stay-in site Download PDF

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TW201709000A
TW201709000A TW104127934A TW104127934A TW201709000A TW 201709000 A TW201709000 A TW 201709000A TW 104127934 A TW104127934 A TW 104127934A TW 104127934 A TW104127934 A TW 104127934A TW 201709000 A TW201709000 A TW 201709000A
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module
service
unmanned aerial
aerial vehicle
vacancy
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TW104127934A
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Chinese (zh)
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TWI561946B (en
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Chuin-Mu Wang
Jian-Hong Liu
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Nat Chin-Yi Univ Of Tech
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Publication of TW201709000A publication Critical patent/TW201709000A/en

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Abstract

The present invention discloses an escort service management method and system for unmanned aerial vehicle. An unmanned aerial vehicle is parked in at advance at a parking location. A vacancy management module records location data of a plurality of stay-in sites and data concerning vacancy or occupation thereof. When an escort service activation trigger module detects a request signal issued by a to-be-escorted vehicle, a trigger signal is generated to allow an escort service control module to retrieve location data of the stay-in sites that are recorded as vacancy from the vacancy management module and obtains a set of aviation control parameters to achieve the stay-in site so as to generate, according to the set of aviation control parameters, a control signal corresponding thereto to an aviation control module to allow the aviation control module to control the unmanned aerial vehicle to fly according to a corresponding aviation path to the corresponding vacant stay-in site. An aviation guide module of an escort guide module issues guide signal during the process of the aviation path to indicate a forwarding path for the to-be-escorted vehicle so as to achieve automatic location-escort guide service function.

Description

無人飛行載具帶位服務管理方法及系統 Unmanned aerial vehicle carrying position service management method and system

本發明係有關一種無人飛行載具帶位服務管理方法及系統,尤指一種可以達到自動帶位的導引服務功能的導引帶位技術。 The invention relates to a method and system for managing the location service of an unmanned aerial vehicle, in particular to a guiding belt technology capable of achieving the automatic guided service function.

隨著汽車數量的激增,加上都會地區可供停車的土地取得不易,導致一般汽車駕駛人在都會地區停車時,總是一位難求,不僅容易造成附近交通的擁擠及紊亂,並且會造成駕駛人心理上極為沉重的負擔與極度的不便困擾。依據目前所知,大多數的收費停車場的停車指引管理機制,大多還是以人力方式提供帶位指引的管理服務,當停車場無空位的停車格時,入口閘道上方的顯示幕則會顯示已無空位的資訊;反之,當停車場有空位的停車格時,縱使入口閘道顯示有空位,但是一般駕駛人卻無法進一步得知空位的停車格所處實際位置以及數量為何?因而無法於第一時間獲悉各停車格的空、佔位狀態資訊,以致會有搶占車位的情事以及容易有危險車安意外情事發生,因而造成駕駛人停車上的不便與困擾。 With the rapid increase in the number of cars and the difficulty in obtaining land available for parking in metropolitan areas, it is always difficult for general motorists to park in metropolitan areas. It is not only easy to cause congestion and disorder in nearby traffic, but also cause The driver’s psychologically heavy burden and extreme inconvenience. As far as we know, most parking guidance management mechanisms for toll parking lots are mostly provided with management services with guidance. When there is no parking space in the parking lot, the display above the entrance gate will show no. Vacancy information; conversely, when the parking lot has a vacant parking space, even if the entrance gate shows vacancies, but the average driver can not further know the actual location and quantity of the vacant parking space? Therefore, it is impossible to know the information of the empty space and the occupancy status of each parking space in the first time, so that there will be a situation in which the parking space is seized and an accidental situation of the dangerous car is likely to occur, thereby causing inconvenience and trouble for the driver to stop.

此外,面積廣闊的露天展覽會場、透天渡假山莊或是透天渡假飯店同樣是以人力方式做帶位指引的服務,於此,一般使用者方能抵達目標展覽位置或是入住飯店的房間。由於以人力方式做帶位指引的服務會有人員管理、情緒控制以及薪資上漲等諸多因素所引發的問題產生,因此,如何開發出一套具備自動化的帶位指引服務技術實已成為相關技術領域業 者所急欲解決克服的技術課題。 In addition, the wide open-air exhibition grounds, the Tiantian Resort or the Tiantian Resort are also guided by the human resources. In this case, the average user can reach the target exhibition location or stay at the hotel. room. As a result of human resources, the services that lead the way will lead to problems caused by many factors such as personnel management, emotional control and salary increases. Therefore, how to develop a set of automated guidance service technology has become a related technical field. industry The company is eager to solve the technical problems that have been overcome.

再者,無論是國防、科學以及商業上,無人飛行載具的應用範圍已經越來越廣泛,許多具有高度危險性或經常性任務已經逐漸由無人飛行載具取代來執行。主要原因是,無人飛行載具有價格低廉與減少人員傷亡的風險等優勢。具體而言,習知之無人飛行載具主要包括三大部份,分別是航空載具、自主飛行系統以及地面導控站。無人飛行載具是依照任務需求的航程、載重、滯空時間選擇合適的機型。自主飛行系統是以系統單晶片整合各種航空感測器(陀螺儀、高度計、電子羅盤等)、飛行控制器、伺服系統、導航系統、無線通訊系統以及電力管理等單元所構成,進而達到自動操控無人飛行載具執行飛行任務之目的。 Furthermore, the use of unmanned aerial vehicles has become more widespread in defense, scientific, and commercial applications, and many highly hazardous or recurring tasks have been gradually replaced by unmanned aerial vehicles. The main reason is that unmanned flight has the advantages of low price and reduced risk of casualties. Specifically, the conventional unmanned aerial vehicle mainly includes three parts, namely, an air vehicle, an autonomous flight system, and a ground navigation station. The unmanned aerial vehicle is selected according to the voyage, load and air time of the mission. The autonomous flight system is composed of a system single chip integrated with various aeronautical sensors (gyro, altimeter, electronic compass, etc.), flight controller, servo system, navigation system, wireless communication system, and power management unit to achieve automatic control. Unmanned aerial vehicles carry out missions.

有鑑於習知技術確實未臻完善,仍然有再改善的必要性,本發明人等乃經不斷的努力研發之下,終於研發出一套有別於上述習知技術與專利的本發明。 In view of the fact that the prior art is not perfect, there is still a need for further improvement, and the inventors have finally developed a set of inventions different from the above-mentioned prior art and patents through continuous efforts.

本發明主要目的在於提供一種無人飛行載具帶位服務管理方法及系統,主要是藉由無人飛行載具與自動帶位服務管理的機能建置,以對面積廣闊的露天停車場、露天展覽會場、透天渡假山莊或是透天渡假飯店提供自動帶位的服務管理,以取代人力式之帶位指引服務,除了可以避免因人員管理、情緒控制以及薪資上漲等諸多因素所致的問題產生之外,並可有效提升帶位服務的管理效能。達成本發明主要目的之技術手段,係將無人飛行載具預先停泊在停泊裝置上;以空位管理模組記錄複數個停滯位置之位址資料及其為空位與佔位的資料;當帶位服務啟動觸發模組感 測到待帶位者發出需求訊號時,產生觸發訊號,以使帶位服務控制模組自該空位管理模組取得記錄為空位的該停滯位置之位址資料,而獲得能抵達該停滯位置的一組航行控制參數,進而依據組航行控制參數產生相對應的控制訊號予飛行控制模組,使飛行控制模組控制無人飛行載具依循對應的航行路徑飛行至對應空位的停滯位置;以帶位指引模組的航行指引模組在航行路徑過程中發出指引訊號,以指引待帶位者前進的路徑。 The main purpose of the present invention is to provide a method and system for managing the location service of an unmanned aerial vehicle, which is mainly constructed by an unmanned aerial vehicle and an automatic location service management, to open a wide open-air parking lot, an open-air exhibition ground, The hotel provides automatic service management to replace the human-based guidance service, in addition to avoiding problems caused by personnel management, emotional control and salary increases. In addition, it can effectively improve the management efficiency of the location service. The technical means for achieving the main object of the present invention is to pre-park the unmanned aerial vehicle on the mooring device; the vacancy management module records the address data of the plurality of stagnant positions and the information of the vacancy and the occupancy; Start trigger module sense When the demand signal is sent, the trigger signal is generated, so that the location service control module obtains the address data of the stagnant position recorded as a vacancy from the vacancy management module, and obtains the address that can reach the stagnant position. a set of navigation control parameters, and then generating a corresponding control signal to the flight control module according to the group navigation control parameters, so that the flight control module controls the unmanned flight vehicle to follow the corresponding navigation path to the stagnation position of the corresponding vacancy; The navigation module of the guidance module issues a guidance signal during the navigation path to guide the path of the person to be carried forward.

10‧‧‧無人飛行載具 10‧‧‧Unmanned aerial vehicle

20‧‧‧帶位服務控制模組 20‧‧‧With service control module

21‧‧‧帶位服務啟動觸發模組 21‧‧‧With service start trigger module

22‧‧‧帶位指引模組 22‧‧‧With Directional Module

23‧‧‧飛行控制模組 23‧‧‧ Flight Control Module

24‧‧‧空位管理模組 24‧‧‧ Vacancy Management Module

210‧‧‧近接感應器 210‧‧‧ proximity sensor

211‧‧‧觸控顯示幕 211‧‧‧ touch display screen

212‧‧‧簡圖 212‧‧‧Simplified

213‧‧‧觸控鈕 213‧‧‧ touch buttons

220‧‧‧航行指引模組 220‧‧‧ Navigation Guide Module

240‧‧‧影像擷取裝置 240‧‧‧Image capture device

241‧‧‧影像處理模組 241‧‧‧Image Processing Module

242‧‧‧空位辨識模組 242‧‧‧ Vacancy Identification Module

243‧‧‧空位匹配模組 243‧‧‧ Vacancy Matching Module

30‧‧‧停泊裝置 30‧‧‧Parking device

31‧‧‧停機棚 31‧‧‧The shed

32‧‧‧載移平台機構 32‧‧‧Transfer platform institutions

40‧‧‧停滯區 40‧‧‧Stagnation zone

41‧‧‧停滯位置 41‧‧‧Stagnation position

Pst‧‧‧起始點 Pst‧‧‧ starting point

Pend‧‧‧目標位置 Pend‧‧‧ Target location

Pn‧‧‧導航點 Pn‧‧‧ navigation point

dn‧‧‧飛行路徑 Dn‧‧‧ flight path

圖1係本發明系統架構的功能方塊實施示意圖。 1 is a schematic diagram of the functional block implementation of the system architecture of the present invention.

圖2係本發明空位管理模組的功能方塊實施示意圖 2 is a schematic diagram of the function block implementation of the vacancy management module of the present invention.

圖3係本發明引導車輛的實施示意圖。 3 is a schematic view showing the implementation of the guided vehicle of the present invention.

圖4係本發明畫面顯示的操控實施示意圖。 FIG. 4 is a schematic diagram of the manipulation implementation of the screen display of the present invention.

圖5係本發明引導車輛進入停車場的實施示意圖。 FIG. 5 is a schematic diagram of the implementation of the present invention for guiding a vehicle into a parking lot.

圖6係本發明停泊裝置的動作實施示意圖。 Fig. 6 is a schematic view showing the operation of the mooring device of the present invention.

圖7係本發明停泊裝置的另一動作實施示意圖。 Fig. 7 is a schematic view showing another embodiment of the operation of the mooring device of the present invention.

圖8係本發明帶位服務的流程控制示意圖。 FIG. 8 is a schematic diagram of flow control of a banded service according to the present invention.

為讓 貴審查委員能進一步瞭解本發明整體的技術特徵與達成本發明目的之技術手段,玆以具體實施例並配合圖式加以詳細說明:請配合參看圖1~4所示為本發明之具體實施例,係包括一無人飛行載具10、一帶位服務控制模組20及一停泊裝置30等技術特徵。帶位服務控制模組20係包括一帶位服務啟動觸發模組21、一帶位指引模組22、一飛行控制模組23及一空位管理模組24。帶位服務啟動觸發模組21 及帶位指引模組22訊號連通。圖5~7所示之停泊裝置30係設在具有複數個停滯位置41的停滯區40的入口處,並將無人飛行載具10預先停泊在停泊裝置30上。該帶位服務控制模組20可預先儲存有分別抵達複數個停滯位置41的航行路徑對應的航行控制參數。該空位管理模組24則記錄複數個停滯位置41之位址資料及其為空位與佔位的資料。該帶位服務啟動觸發模組21感測是否有待帶位者發出一需求訊號;當帶位服務啟動觸發模組21感測到需求訊號時,便產生一觸發訊號,帶位服務控制模組20接收觸發訊號,並自空位管理模組24取得記錄為空位的停滯位置41之位址資料,而獲得能抵達停滯位置41的一組航行控制參數,進而依據該組航行控制參數產生相對應的控制訊號予飛行控制模組23;該飛行控制模組23再依據控制訊號控制無人飛行載具10依循對應的航行路徑飛行至對應空位的停滯位置41;接著,再以帶位指引模組22的航行指引模組220在航行路徑過程中發出指引訊號(如歡迎詞、左轉、直行、右轉、暫停等待、抵達目標位置以及致謝詞等),藉以指引待帶位者前進的路徑;緊接著,當無人飛行載具10抵達對應的停滯位置41後,則完成本次帶位服務飛行,該空位管理模組24則將停滯位置41更改記錄為佔位資料;緊接著,飛行控制模組23再控制無人飛行載具10返回停泊裝置30並做停泊。 In order to allow the reviewing committee to further understand the technical features of the present invention and the technical means for achieving the object of the present invention, it will be described in detail by way of specific embodiments and drawings: please refer to FIG. 1 to FIG. The embodiment includes technical features such as an unmanned aerial vehicle 10, a belt service control module 20, and a mooring device 30. The locating service control module 20 includes a locating service activation triggering module 21, a locating guidance module 22, a flight control module 23, and a vacancy management module 24. Band service start trigger module 21 And the position guiding module 22 signal is connected. The mooring device 30 shown in Figures 5-7 is located at the entrance of the stagnation zone 40 having a plurality of stagnant positions 41, and the unmanned aerial vehicle 10 is pre-parked on the mooring device 30. The carry-on service control module 20 may pre-store navigation control parameters corresponding to the navigation paths respectively reaching the plurality of stagnant positions 41. The vacancy management module 24 records the address data of the plurality of stagnant locations 41 and the data of the vacancy and the occupancy. The presence service trigger module 21 senses whether a candidate is to send a demand signal; when the service start trigger module 21 senses the demand signal, a trigger signal is generated, and the service control module 20 is provided. Receiving the trigger signal, and obtaining the address data of the stagnant position 41 recorded as a vacancy from the vacancy management module 24, and obtaining a set of navigation control parameters that can reach the stagnation position 41, and generating corresponding control according to the set of navigation control parameters. The signal is transmitted to the flight control module 23; the flight control module 23 then controls the unmanned aerial vehicle 10 to follow the corresponding navigation path to the stagnation position 41 of the corresponding vacancy according to the control signal; The guiding module 220 issues a guiding signal (such as a welcome word, a left turn, a straight line, a right turn, a pause wait, a arrival target position, and a thank-you word) during the navigation path, thereby guiding the path of the person to be carried forward; When the unmanned aerial vehicle 10 arrives at the corresponding stagnant position 41, the current service flight is completed, and the vacancy management module 24 changes the stagnant position 41 to record. Placeholder data; Then, control module 23 and then control the flight unmanned aerial vehicle parking means 30 and 10 return to make parking.

具體來說,帶位服務啟動觸發模組21係包括一近接感應器210,該近接感應器210可設置在無人飛行載具10,如圖3所示;或是停泊裝置30上,如圖6、7所示。圖5所示的實施例中,當待帶位者靠近入口處時,該帶位指引模組22之一空位顯示模組(圖未示)則自空位管理模組24取得空位記錄而顯示是否有空位;當待帶位者自行確認有空位,則可發出上述之需求訊號,於是,帶位服務啟動觸發模組21即可產生上述之觸發訊號。 此外,圖6、7所示之停泊裝置30係包含一停機棚31、一載移平台機構32及一動力驅動機構(圖未示)。該停機棚31可供無人飛行載具10停置,動力驅動機構(如馬達、皮帶及齒輪組的組合;或是線性致動組件)可受帶位服務控制模組20的控制而驅動載移平台機構32往位於停機棚31內的第一位置或是往位於停機棚31外的第二位置移動,當該觸發訊號產生時,載移平台機構32則自第一位置移往第二位置,當無人飛行載具10完成本次帶位而降落在載移平台機構32時,如圖6所示,該載移平台機構32則自第二位置移往第一位置,如圖7所示,於此,即可達到使無人飛行載具10達到遮蔽的防雨功效;不僅如此,本發明亦可於停機棚31設置充電模組,以對無人飛行載具10之電力系統進行充電。 Specifically, the location service activation trigger module 21 includes a proximity sensor 210, which may be disposed on the unmanned aerial vehicle 10, as shown in FIG. 3; or on the parking device 30, as shown in FIG. 7, shows. In the embodiment shown in FIG. 5, when the person to be positioned is close to the entrance, a vacant display module (not shown) of the locating guide module 22 obtains a vacancy record from the vacancy management module 24 to display whether If there is a vacancy, the above-mentioned demand signal can be issued, and the triggering module 21 can be activated to generate the trigger signal. In addition, the mooring device 30 shown in FIGS. 6 and 7 includes a parking shed 31, a loading platform mechanism 32, and a power driving mechanism (not shown). The awning 31 can be used for the unmanned aerial vehicle 10 to be parked, and the power drive mechanism (such as a combination of a motor, a belt and a gear set; or a linear actuating assembly) can be driven by the belt service control module 20 to drive the shift. The platform mechanism 32 moves to a first position in the awning 31 or to a second position outside the awning 31. When the trigger signal is generated, the loading platform mechanism 32 moves from the first position to the second position. When the unmanned aerial vehicle 10 completes the current position and land on the loading platform mechanism 32, as shown in FIG. 6, the loading platform mechanism 32 moves from the second position to the first position, as shown in FIG. In this way, the rain protection effect of the unmanned aerial vehicle 10 can be achieved. Moreover, the present invention can also provide a charging module in the parking shed 31 to charge the power system of the unmanned aerial vehicle 10.

請參看圖2所示之空位管理模組24係包括一影像擷取裝置240、一影像處理模組241及一空位辨識模組242。影像擷取裝置240設置在無人飛行載具10上,如圖3所示。空位管理模組24於一預定時間產生一空位檢視需求訊號,飛行控制模組23依據空位檢視需求訊號控制無人飛行載具10於停滯區40巡航,影像擷取裝置240擷取停滯區40的即時影像,該影像處理模組241將停滯區40影像與預存的停滯區40的基準影像比對以獲得停滯位置41之位址資料及其空位資料。此外,圖2所示之空位管理模組24更包括一空位匹配模組243;當帶位服務啟動觸發模組21感測待帶位者所發出的需求訊號時,以影像擷取裝置240擷取待帶位者的影像,影像處理模組241將待帶位者影像與預存的一尺寸基準影像比對以獲得待帶位者的尺寸資訊(如車輛尺寸或是住宿人員數量);當帶位服務啟動觸發模組21感測到需求訊號時,便產生一觸發訊號,帶位服務控制模組20接收觸發訊 號,並經由空位匹配模組243而自空位管理模組24取得待帶位者的尺寸資訊相匹配且記錄為空位的停滯位置41之位址資料,而獲得能抵達與待帶位者的尺寸資訊相匹配之停滯位置41(如停車格或是住宿房間)的一組航行控制參數,進而依據該組航行控制參數產生相對應的控制訊號予飛行控制模組23;該飛行控制模組23依據控制訊號控制無人飛行載具10依循對應的航行路徑飛行至對應空位的停滯位置41。 The vacancy management module 24 shown in FIG. 2 includes an image capture device 240, an image processing module 241, and a vacancy recognition module 242. The image capturing device 240 is disposed on the unmanned aerial vehicle 10 as shown in FIG. The vacancy management module 24 generates a vacancy inspection demand signal at a predetermined time. The flight control module 23 controls the unmanned aerial vehicle 10 to cruise in the stagnation zone 40 according to the vacancy inspection demand signal, and the image capturing device 240 captures the stagnation zone 40. The image processing module 241 compares the image of the stagnant zone 40 with the reference image of the pre-stored stagnant zone 40 to obtain the address data of the stagnant location 41 and its vacancy data. In addition, the vacancy management module 24 shown in FIG. 2 further includes a vacancy matching module 243. When the locating service activation triggering module 21 senses the demand signal sent by the occupant, the image capturing device 240 撷Taking the image of the occupant, the image processing module 241 compares the image of the occupant with the pre-stored one-size reference image to obtain the size information of the person to be occupant (such as the size of the vehicle or the number of accommodation personnel); When the service start trigger module 21 senses the demand signal, a trigger signal is generated, and the bit service control module 20 receives the trigger signal. And obtaining, by the vacancy matching module 243, the address information of the stagnation position 41 that matches the size information of the person to be occupant and recorded as a vacancy, and obtains the size of the stagnation position to be occupied. a set of navigation control parameters of the stagnant position 41 (such as a parking space or a living room) matched by the information, and then generating a corresponding control signal to the flight control module 23 according to the navigation control parameters; the flight control module 23 is based on The control signal controls the unmanned aerial vehicle 10 to follow the corresponding navigation path to the stagnant position 41 of the corresponding vacancy.

如圖5~7所示之帶位服務啟動觸發模組21係包括一觸控顯示幕211,該觸控顯示幕211顯示有對應停滯區40及複數個停滯位置41的一簡圖212,且當停滯位置41為空位時,於簡圖212上顯示出對應於為空位的停滯位置41的觸控鈕213;當待帶位者按壓觸控鈕213時,即為發出該需求訊號,該帶位服務啟動觸發模組21便產生該觸發訊號。至於本發明帶位服務的具體流程控制示意則如圖8所示。 The touch-enabled service activation triggering module 21 shown in FIGS. 5-7 includes a touch display screen 211, and the touch display screen 211 displays a schematic diagram 212 corresponding to the stagnant zone 40 and the plurality of stagnant locations 41, and When the stagnant position 41 is vacant, the touch button 213 corresponding to the stagnation position 41 that is vacant is displayed on the schematic diagram 212; when the touch button 213 is pressed, the demand signal is sent. The bit service start trigger module 21 generates the trigger signal. The specific flow control diagram of the location-based service of the present invention is shown in FIG.

此外,帶位服務控制模組20可裝設在無人飛行載具10上;或是設在地面管制站上;於裝設在無人飛行載具10的實施例中,可將複數停滯位置41的複數組航行控制參數預先輸出至帶位服務控制模組20中,以執行上述的自動帶位服務飛行。另於裝設在地面管制站的實施例中,可將複數停滯位置41對應的複數組航行控制參數預先輸入於帶位服務控制模組20(如電腦、智慧型手機或是平板電腦等)中,再透過無線通訊模組(如無線區域網路WIFI模組、行動通訊模組或是無線射頻通訊模組)使無人飛行載具10上之自主飛行系統與帶位服務控制模組20訊號連通,以將上述控制訊號依序傳輸至無人飛行載具10,進而實現上述的自動帶位服務飛行。 In addition, the locating service control module 20 can be mounted on the unmanned aerial vehicle 10 or on the ground control station; in the embodiment of the unmanned aerial vehicle 10, the plurality of stagnant positions 41 can be The complex array navigation control parameters are pre-outputted to the location service control module 20 to perform the automatic location service flight described above. In another embodiment of the ground control station, the complex array navigation control parameters corresponding to the plurality of stagnant positions 41 can be pre-inputted into the location service control module 20 (such as a computer, a smart phone or a tablet). And then, through the wireless communication module (such as the wireless local area network WIFI module, the mobile communication module or the wireless RF communication module), the autonomous flight system on the unmanned aerial vehicle 10 is connected with the position service control module 20 signal. In order to sequentially transmit the above control signals to the unmanned aerial vehicle 10, the above-mentioned automatic location service flight is realized.

具體來說,本發明無人飛行載具10在執行自動帶位服務飛 行之前會先執行一飛行路徑教導飛行,換言之,即於執行帶位服務模式飛行之前的航行參數學習步驟,具體的做法,係透過無線通訊模組控制無人飛行載具10依序飛過各飛行路徑dn,每一飛行路徑dn包含一起始點Pst(即停泊裝置30位置)、一目標位置Pend(即選定之停滯位置)及位於起始點Pst與目標位置Pend之間的複數導航點Pn,帶位服務控制模組20則將每一飛行路徑dn之飛行資料(如座標參數、高度參數或是時間參數等)依序記錄為一組航行控制參數,每一組航行控制參數則包含起始點Pst、目標位置Pend及導航點Pn的座標參數、高度參數、速度參數、方向參數、時間參數以及運轉參數。 Specifically, the unmanned aerial vehicle 10 of the present invention performs an automatic take-off service flight Before the trip, a flight path teaching flight will be executed first, in other words, the navigation parameter learning step before the flight mode service mode is executed. The specific method is to control the unmanned aerial vehicle 10 to fly through each flight through the wireless communication module. Path dn, each flight path dn includes a starting point Pst (ie, the position of the mooring device 30), a target position Pend (ie, the selected stagnant position), and a plurality of navigation points Pn between the starting point Pst and the target position Pend, The position service control module 20 sequentially records the flight data (such as coordinate parameters, height parameters or time parameters) of each flight path dn as a set of navigation control parameters, and each group of navigation control parameters includes a start. Point coordinates, height parameters, speed parameters, direction parameters, time parameters, and operating parameters of point Pst, target position Pend, and navigation point Pn.

請參看圖4、5所示的運作實施例,假設車輛欲停車而靠近入口處時,入口處附近設有一可供車輛駕駛操控觸的觸控顯示幕211,且顯示有對應停滯區40及複數個停滯位置41的簡圖212,當車輛駕駛欲選定簡圖212上之空位停車格D5時,則可直接按壓位於簡圖212上所顯示的停車格D5的觸控鈕213,於此,即可發出代表停車格D5為空位的需求訊號,當帶位服務啟動觸發模組21感應或接收到需求訊號時,則產生觸發訊號,帶位服務控制模組20接收觸發訊號,並自空位管理模組24取得記錄停車格D5的停滯位置41之位址資料,以獲得能抵達該停滯位置41的一組航行控制參數,進而依據該組航行控制參數產生相對應的控制訊號予飛行控制模組23,該飛行控制模組23依據控制訊號控制無人飛行載具10依循對應的航行路徑飛行至停車格D5的停滯位置41,於飛行過程中,帶位指引模組22的航行指引模組220在航行路徑過程中發出指引訊號(如歡迎詞、左轉、直行、右轉、暫停等待、抵達目標位置以及致謝詞等),當無人飛行載具10 抵達停車格D5位置後,則完成本次的帶位服務飛行,此時,空位管理模組24則將停車格D5位置更改記錄為佔位資料,於是飛行控制模組23再控制無人行載具返回停泊裝置30並做停泊,此外,在飛行的過程中,無人飛行載具10依據該組航行控制參數所預定之高度、速度及飛行路徑dn自起始點Pst經導航點P1而航向目標位置Pend後,再自目標位置Pend1返回至起始點Pst,而飛行路徑dn為路徑dD51、路徑dD52及路徑dD53的組合,亦即dn=dD51+dD52+dD53,另外,當無人飛行載具10自起始點Pst航向導航點P1時,帶位服務控制模組20則讀取該組航行控制參數中之高度參數、方向參數及速度參數,並與飛行運轉參數一同運算而產生用以控制無人飛行載具10飛行運轉的控制訊號,並依據控制訊號的控制而做路徑dD51的飛行,於此,即可航向導航點P1;當無人飛行載具1010抵達導航點P1時,則比對無人飛行載具10所處座標是否與導航點P1的座標參數符合,判斷結果為是,帶位服務控制模組20則讀取導航點P1之高度參數、方向參數及速度參數,並與飛行運轉參數一同運算而產生用以控制無人飛行載具10飛行運轉的控制訊號,並依據控制訊號的控制而做路徑dD52的飛行,於此,即可航向目標位置Pend;當無人飛行載具10即將抵達起始點Pst1時,則比對無人飛行載具10所處座標是否與起始點Pst的座標參數符合,判斷結果為是,則控制無人飛行載具10降落在起始點Pst(即停泊裝置30位置)的位置上。 Referring to the working embodiment shown in FIG. 4 and FIG. 5, assuming that the vehicle is to be parked near the entrance, a touch display screen 211 for driving and controlling the vehicle is provided near the entrance, and the corresponding stagnant area 40 and plural are displayed. A schematic diagram 212 of the stagnant position 41, when the vehicle is driving to select the vacant parking space D5 on the sketch 212, the touch button 213 of the parking space D5 displayed on the schematic 212 can be directly pressed, where A demand signal indicating that the parking space D5 is vacant may be issued. When the service start trigger module 21 senses or receives the demand signal, a trigger signal is generated, and the bit service control module 20 receives the trigger signal, and the vacancy management mode The group 24 obtains the address data of the stagnant position 41 of the parking space D5 to obtain a set of navigation control parameters that can reach the stagnant position 41, and generates corresponding control signals to the flight control module 23 according to the set of navigation control parameters. The flight control module 23 controls the unmanned aerial vehicle 10 to follow the corresponding navigation path to the stagnation position 41 of the parking space D5 according to the control signal. During the flight, the positioning guidance module 22 The line guidance module 220 issues a guidance signal (such as a welcome word, a left turn, a straight line, a right turn, a pause wait, an arrival target position, and a thank-you note) during the navigation path, and when the unmanned aerial vehicle 10 arrives at the parking space D5 position Then, the current service flight is completed. At this time, the vacancy management module 24 records the change of the parking space D5 as the placeholder data, and then the flight control module 23 controls the unmanned vehicle to return to the parking device 30 and does Mooring, in addition, during the flight, the unmanned aerial vehicle 10 according to the set of navigation control parameters of the predetermined height, speed and flight path dn from the starting point Pst through the navigation point P 1 and heading to the target position Pend, and then The target position Pend 1 returns to the starting point Pst, and the flight path dn is a combination of the path dD5 1 , the path dD5 2 and the path dD5 3 , that is, dn=dD5 1 +dD5 2 +dD5 3 , in addition, when the unmanned flying vehicle Pst heading from the starting point 10 the navigation points P 1, the tape position control service module 20 reads the set of parameters to control the height of navigation parameters, the parameters of speed and direction parameter, and calculating with the flight operating parameters to produce Control no The human flight vehicle 10 controls the flight operation and performs the flight of the path dD5 1 according to the control of the control signal. Here, the navigation navigation point P 1 can be used; when the unmanned aerial vehicle 1010 reaches the navigation point P 1 , then match UAV 10 which meets the navigation coordinate point P coordinates set to 1. the determination result is yes, the service control module with bit 20 of the navigation point height parameter P 1, the direction and speed parameters is read parameters, And generating a control signal for controlling the flight operation of the unmanned aerial vehicle 10 together with the flight operation parameter, and performing the flight of the path dD5 2 according to the control of the control signal, thereby, the heading position Pend; when no one is flying When the carrier 10 is about to arrive at the starting point Pst 1 , it is compared with whether the coordinate of the unmanned aerial vehicle 10 coincides with the coordinate parameter of the starting point Pst, and if the judgment result is yes, the unmanned flying vehicle 10 is controlled to land at the start. Point Pst (ie the position of the mooring device 30).

因此,藉由上述具體實施例的說明,本發明確實可藉由無人飛行載具與自動帶位服務管理的機能建置,以對面積廣闊的露天停車場、露天展覽會場、透天渡假山莊或是透天渡假飯店提供自動帶位的服務管理,以取代人力式之帶位指引服務,除了可以避免因人員管理、情緒控制 以及薪資上漲等諸多因素所致的問題產生之外,並可有效提升帶位服務的管理效能。 Therefore, with the above description of the specific embodiments, the present invention can be constructed by the functions of unmanned aerial vehicles and automatic location service management, for a wide open-air parking lot, an open-air exhibition ground, a through-the-sky resort or It is the automatic management service provided by the hotel to replace the human-oriented guidance service, in addition to avoiding personnel management and emotional control. In addition to the problems caused by many factors such as salary increases, and can effectively improve the management efficiency of the location service.

以上所述,僅為本發明之可行實施例,並非用以限定本發明之專利範圍,凡舉依據下列請求項所述之內容、特徵以及其精神而為之其他變化的等效實施,皆應包含於本發明之專利範圍內。本發明所具體界定於請求項之結構特徵,未見於同類物品,且具實用性與進步性,已符合發明專利要件,爰依法具文提出申請,謹請 鈞局依法核予專利,以維護本申請人合法之權益。 The above is only a possible embodiment of the present invention, and is not intended to limit the scope of the patents of the present invention, and the equivalent implementations of other changes according to the contents, features and spirits of the following claims should be It is included in the patent of the present invention. The invention is specifically defined in the structural features of the request item, is not found in the same kind of articles, and has practicality and progress, has met the requirements of the invention patent, and has filed an application according to law, and invites the bureau to approve the patent according to law to maintain the present invention. The legal rights of the applicant.

10‧‧‧無人飛行載具 10‧‧‧Unmanned aerial vehicle

20‧‧‧帶位服務控制模組 20‧‧‧With service control module

21‧‧‧帶位服務啟動觸發模組 21‧‧‧With service start trigger module

22‧‧‧帶位指引模組 22‧‧‧With Directional Module

2‧‧‧飛行控制模組 2‧‧‧ Flight Control Module

24‧‧‧空位管理模組 24‧‧‧ Vacancy Management Module

30‧‧‧停泊裝置 30‧‧‧Parking device

Claims (10)

一種無人飛行載具帶位服務管理方法,其包括:提供一無人飛行載具、一帶位服務控制模組及一停泊裝置;該帶位服務控制模組包括一帶位服務啟動觸發模組、一帶位指引模組、一飛行控制模組及一空位管理模組;該帶位服務啟動觸發模組及該帶位指引模組訊號連通;將該停泊裝置設在具有複數個停滯位置的一停滯區之一入口處,並將該無人飛行載具預先停泊在該停泊裝置上;以該帶位服務控制模組預先儲存有分別抵達該複數個停滯位置的航行路徑對應的航行控制參數;以該空位管理模組記錄該複數個停滯位置之位址資料及其為空位與佔位的資料;以該帶位服務啟動觸發模組感測是否有待帶位者發出一需求訊號;當該帶位服務啟動觸發模組感測到該需求訊號時,便產生一觸發訊號,該帶位服務控制模組接收該觸發訊號,並自該空位管理模組取得記錄為空位的該停滯位置之位址資料,而獲得能抵達該停滯位置的一組航行控制參數,進而依據該組航行控制參數產生相對應的控制訊號予該飛行控制模組;該飛行控制模組依據該控制訊號控制該無人飛行載具依循對應的航行路徑飛行至對應空位的該停滯位置;以該帶位指引模組的一航行指引模組在航行路徑過程中發出指引訊號,以指引該待帶位者前進的路徑;當該無人行載具抵達對應的該停滯位置後,完成本次帶位,該空位管理模組將該停滯位置更改記錄為佔位資料;該飛行控制模組再控制該無人行載具返回該停泊裝置並做停泊。 A method for managing an unmanned aerial vehicle with a position service includes: providing an unmanned aerial vehicle, a service control module with a position and a parking device; the service control module with a position service includes a start-up trigger module with a service, and a belt position a pilot module, a flight control module and a vacancy management module; the locating service activation triggering module and the locating guidance module signal communication; the parking device is disposed in a stagnation zone having a plurality of stagnant positions An entrance, and the unmanned aerial vehicle is pre-parked on the mooring device; the navigation service control module pre-stores navigation control parameters corresponding to the navigation paths respectively reaching the plurality of stagnant positions; The module records the address data of the plurality of stagnant positions and the data of the vacancy and the placeholder; and the triggering module of the band service starts to sense whether the user needs to send a demand signal; when the band service starts to trigger When the module senses the demand signal, a trigger signal is generated, and the band service control module receives the trigger signal and obtains a record from the space management module. Obtaining a set of navigation control parameters that can reach the stagnant position, and generating a corresponding control signal according to the set of navigation control parameters to the flight control module; the flight control module Controlling the unmanned aerial vehicle to follow the corresponding navigation path to the stagnation position of the corresponding vacant space according to the control signal; a navigation guidance module of the directional guidance module issues a guidance signal during the navigation path to guide the waiting The path of the forwarder; when the unmanned vehicle arrives at the corresponding stagnant position, the current position is completed, and the vacancy management module records the stagnation position change as the placeholder data; the flight control module re-controls The unmanned vehicle returns to the mooring device and is parked. 如請求項1所述之無人飛行載具帶位服務管理方法,其中,該帶位服務啟動觸發模組包括一近接感應器,該近接感應器是位於該入口處來感測是否有待帶位者靠近,當感測到有待帶位者靠近時,該帶位指引模組的一空位顯示模組則自該空位管理模組取得空位記錄而顯示是否有空位;當該待帶位者自行確認有空位,並發出該需求訊號,該帶位服務啟動觸發模組便產生該觸發訊號。 The unmanned aerial vehicle carrier service management method of claim 1, wherein the location service activation triggering module comprises a proximity sensor, the proximity sensor is located at the entrance to sense whether the user is to be taken Closely, when it is sensed that the person to be brought closer is approaching, a vacant display module of the locating guide module obtains a vacancy record from the vacancy management module to indicate whether there is a vacancy; The vacancy is issued and the demand signal is sent, and the trigger service module activates the trigger module to generate the trigger signal. 如請求項2所述之無人飛行載具帶位服務管理方法,其中,該近接感應器設置在該無人飛行載具上。 The unmanned aerial vehicle carrier position service management method of claim 2, wherein the proximity sensor is disposed on the unmanned aerial vehicle. 如請求項1所述之無人飛行載具帶位服務管理方法,其中,該空位管理模組包括一影像擷取裝置、一影像處理模組及一空位辨識模組;該影像擷取裝置設置在該無人飛行載具上;該空位管理模組於一預定時間產生一空位檢視需求訊號,該飛行控制模組依據該空位檢視需求訊號控制該無人飛行載具於該停滯區巡航,該影像擷取裝置擷取該停滯區的即時影像,該影像處理模組將該停滯區影像與預存的該停滯區的基準影像比對以獲得該停滯位置之位址資料及其空位資料。 The method of managing an unmanned aerial vehicle with a position service according to claim 1, wherein the vacancy management module comprises an image capture device, an image processing module and a vacancy recognition module; the image capture device is disposed at The vacancy management module generates a vacancy inspection demand signal at a predetermined time, and the flight control module controls the unmanned aerial vehicle to cruise in the stagnation zone according to the vacancy inspection demand signal, and the image capture system The device captures the real-time image of the stagnant area, and the image processing module compares the image of the stagnant area with the pre-stored reference image of the stagnant area to obtain the address data of the stagnant position and the vacancy data thereof. 如請求項4所述之無人飛行載具帶位服務管理方法,其中,該空位管理模組更包括一空位匹配模組;當該帶位服務啟動觸發模組感測該待帶位者所發出的該需求訊號時,以該影像擷取裝置擷取該待帶位者的影像,該影像處理模組將該待帶位者影像與預存的一尺寸基準影像比對以獲得該待帶位者的尺寸資訊;當該帶位服務啟動觸發模組感測到該需求訊號時,便產生一觸發訊號,該帶位服務控制模組接收該觸發訊號,並經由該空位匹配模組而自該空位管理模組取得與該待帶位者的尺寸資訊相匹配且記錄為空位的該停滯位置之位址資料,而獲得能抵達與該待帶位者的尺寸資訊相匹配之該停滯位置的一組航行控制參數,進而依據該組航行控制參數產 生相對應的控制訊號予該飛行控制模組;該飛行控制模組依據該控制訊號控制該無人飛行載具依循對應的航行路徑飛行至對應空位的該停滯位置。 The unmanned aerial vehicle carrier service management method according to claim 4, wherein the vacancy management module further includes a vacancy matching module; and the locating service activation triggering module senses the person to be borne The image capturing device captures the image of the person to be taped by the image capturing device, and the image processing module compares the image of the person to be taped with the pre-stored one-size reference image to obtain the person to be taped. The size information is generated. When the demanding service triggering module senses the demand signal, a trigger signal is generated, and the tape service control module receives the trigger signal, and the space is replaced by the space matching module. The management module obtains the address data of the stagnant position that matches the size information of the to-be-positioned person and records the space as a vacancy, and obtains a set of the stagnant position that can reach the size information matching the size information of the to-be-positioned person. Navigation control parameters, and then based on the set of navigation control parameters The corresponding control signal is sent to the flight control module. The flight control module controls the unmanned aerial vehicle to follow the corresponding navigation path to the stagnant position of the corresponding vacancy according to the control signal. 如請求項4所述之無人飛行載具帶位服務管理方法,其中,該帶位服務啟動觸發模組包括一觸控顯示幕,該觸控顯示幕顯示有對應該停滯區及該複數個停滯位置的一簡圖,且當該停滯位置為空位時,於該簡圖上顯示出對應於為空位的該停滯位置的觸控鈕;當該待帶位者按壓該觸控鈕時,即為發出該需求訊號,該帶位服務啟動觸發模組便產生該觸發訊號。 The method for managing an unmanned aerial vehicle with a position service according to claim 4, wherein the activation service triggering module includes a touch display screen, and the touch display screen displays a corresponding stagnant zone and the plurality of stagnant a schematic diagram of the location, and when the stagnant position is vacant, the touch button corresponding to the stagnant position that is vacant is displayed on the diagram; when the to-be-positioned person presses the touch button, The demand signal is sent, and the trigger service module generates the trigger signal. 如請求項1所述之無人飛行載具帶位服務管理方法,其中,該停泊裝置包含一停機棚、一載移平台機構及一動力驅動機構,該停機棚可供該無人飛行載具停置,該動力驅動機構可受該帶位服務控制模組的控制而驅動該載移平台機構往位於該停機棚內的第一位置及往位於該停機棚外的第二位置移動,當該觸發訊號產生時,該載移平台機構則自該第一位置移往該第二位置,當無人飛行載具完成本次帶位而降落在該載移平台機構時,該載移平台機構則自該第二位置移往該第一位置。 The unmanned aerial vehicle position management service method of claim 1, wherein the parking device comprises a parking shed, a loading platform mechanism and a power driving mechanism, wherein the parking shed can be used to park the unmanned aerial vehicle The power drive mechanism can be driven by the position service control module to drive the load platform mechanism to move to a first position in the awning and to a second position outside the awning, when the trigger signal When generated, the loading platform mechanism moves from the first position to the second position, and when the unmanned aerial vehicle completes the current position and landed on the loading platform mechanism, the loading platform mechanism is from the first The two positions are moved to the first position. 一種無人飛行載具帶位服務管理系統,其包括:一無人飛行載具;一停泊裝置,其設在具有複數個停滯位置的一停滯區之一入口處,以供該無人飛行載具預先停泊;及一帶位服務控制模組,其包括一帶位服務啟動觸發模組、一帶位指引模組、一飛行控制模組及一空位管理模組;該帶位服務啟動觸發模組及該帶位指引模組訊號連通,該帶位服務控制模組預先儲存有分別抵達該複數個停滯位置的航行路徑對應的航行控制參數;該空位管理模組記錄該複數個停滯位置之位址資料及其為空位與佔位的資料;該帶位服務啟動觸發模組感測是否有待帶位者發出一需求訊號;當該帶位服務啟動觸發模組感測 到該需求訊號時,便產生一觸發訊號,該帶位服務控制模組接收該觸發訊號,並自該空位管理模組取得記錄為空位的該停滯位置之位址資料,而獲得能抵達該停滯位置的一組航行控制參數,進而依據該組航行控制參數產生相對應的控制訊號予該飛行控制模組;該飛行控制模組依據該控制訊號控制該無人飛行載具依循對應的航行路徑飛行至對應空位的該停滯位置;該帶位指引模組的一航行指引模組在航行路徑過程中發出指引訊號,以指引該待帶位者前進的路徑;當該無人行載具抵達對應的該停滯位置後,完成本次帶位,該空位管理模組將該停滯位置更改記錄為佔位資料;該飛行控制模組再控制該無人行載具返回該停泊裝置並做停泊。 An unmanned aerial vehicle carrying service management system comprising: an unmanned aerial vehicle; a parking device disposed at an entrance of a stagnant zone having a plurality of stagnant positions for pre-parking the unmanned aerial vehicle And a service control module, including a service start trigger module, a position guide module, a flight control module and a vacancy management module; the service start trigger module and the position guide The module signal communication module is pre-stored with navigation control parameters corresponding to the navigation paths respectively reaching the plurality of stagnant positions; the space management module records the address data of the plurality of stagnant positions and is vacant And the information of the placeholder; the band service start trigger module senses whether the person to be charged sends a demand signal; when the band service starts trigger module sensing When the demand signal is received, a trigger signal is generated, and the location service control module receives the trigger signal, and obtains the address data of the stagnant position recorded as a vacancy from the vacancy management module, and obtains the stagnation of the stagnation position. a set of navigation control parameters of the position, and correspondingly generating a corresponding control signal to the flight control module according to the set of navigation control parameters; the flight control module controls the unmanned aerial vehicle to follow the corresponding navigation path according to the control signal to Corresponding to the stagnation position of the vacancy; the navigation guidance module of the locating guide module sends a guidance signal during the navigation path to guide the path of the person to be carried forward; when the unmanned vehicle arrives at the corresponding stagnation After the location, the current location is completed, and the vacancy management module records the stagnation position change as the placeholder data; the flight control module then controls the unmanned vehicle to return to the berthing device and perform parking. 如請求項8所述之無人飛行載具帶位服務管理系統,其中,該帶位服務啟動觸發模組包括一近接感應器,該近接感應器是位於該入口處來感測是否有待帶位者靠近,當感測到有待帶位者靠近時,該帶位指引模組的一空位顯示模組則自該空位管理模組取得空位記錄而顯示是否有空位;當該待帶位者自行確認有空位,並發出該需求訊號,該帶位服務啟動觸發模組便產生該觸發訊號。 The unmanned aerial vehicle carrier service management system of claim 8, wherein the location service activation triggering module comprises a proximity sensor, the proximity sensor is located at the entrance to sense whether a person is to be taken Closely, when it is sensed that the person to be brought closer is approaching, a vacant display module of the locating guide module obtains a vacancy record from the vacancy management module to indicate whether there is a vacancy; The vacancy is issued and the demand signal is sent, and the trigger service module activates the trigger module to generate the trigger signal. 如請求項8所述之無人飛行載具帶位服務管理系統,其中,該停泊裝置包含一停機棚、一載移平台機構及一動力驅動機構,該停機棚可供該無人飛行載具停置,該動力驅動機構可受該帶位服務控制模組的控制而驅動該載移平台機構往位於該停機棚內的第一位置及往位於該停機棚外的第二位置移動,當該觸發訊號產生時,該載移平台機構則自該第一位置移往該第二位置,當無人飛行載具完成本次帶位而降落在該載移平台機構時,該載移平台機構則自該第二位置移往該第一位置。 The unmanned aerial vehicle position service management system of claim 8, wherein the parking device comprises a parking shed, a loading platform mechanism and a power driving mechanism, wherein the parking shed can be used to park the unmanned aerial vehicle The power drive mechanism can be driven by the position service control module to drive the load platform mechanism to move to a first position in the awning and to a second position outside the awning, when the trigger signal When generated, the loading platform mechanism moves from the first position to the second position, and when the unmanned aerial vehicle completes the current position and landed on the loading platform mechanism, the loading platform mechanism is from the first The two positions are moved to the first position.
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