M290485 八、新型說明： 【新型所屬之技術領域】 ㈣行修正控制裝置，尤指-種接 號’以控制該飛行器飛行 ：❼己錄而輪出修正控制訊 【先前技術】 “„„之域修正㈣裝置者。 按，一般遙控飛機'遙控直昇 盔 一^ 教育意義’但入門卻頗為不易：因有科學 α彺彺先侍砸下大把的金錢以換取教訓。 1 口此而要「種飛行器之飛行修正控制裝置，其以-個維度為 ::所:接I收到遙控器所發出之原始控制訊號時，可根據加速度减 測益所感測之加衫G值並參考該記憶體中之飛行記錄 1 t控制訊號，以控制該飛行器飛行，用以提供學習飛行或嘗試自動 氣航控制之玩家-個馬上可取得之穩定位置控制的平台。 【新型内容】 本創作之-目的係提供一種飛行器之飛行修正控制裝置，其以 -個維度為單位，於接收到遙控器所發出之原始控制訊號時，^根 據加速度感測器所感測之加速度G值並參考該記憶體中之飛行記 錄=輸出修正控制訊號，以控制該飛行器飛行，用以提供學習飛^ 或I试自動飛航控制之玩家一個馬上可取得之穩定位置控制的平 台0 為達上述之目的，本創作之飛行器之飛行修正控制裝置，該飛 行至y具有動力機組、一遙控态、一接收端及一降落機制，該 飛行修正控制裝置包括··一加速度感測器，其可感測及計算一飛行 器飛行時之加速度；一類比/數位轉換器，耦接至該加速度感測器， 可將該加速度感測器所感測之加速度轉換成數位型式；一微控制 5 M290485 器’耦接至該類比/數位轉換器，其可 加以處理；一記情I#，耦接$ H ^立型式之加速度並 …體辆接至相控制器，可供儲存該飛行哭之飛 ^二及：參嫩通訊介面，轉接至該微控制器， 二：：：：：#作拉式或路規劃’·俾該微控制器接收到該遙 疋/又U值亚麥考该圮憶體中之飛 號，以控制該飛行器之飛行。而輸出—修正控制訊 為使、貴審查委員能進一步瞭解本創作之結構、特徵及其目 、餘附以圖式及較佳具體實施例之詳細說明如产。 【實施方式】 σ 請參照圖1，其緣示本幸土眘f 7^ 财署夕…立 例之飛行器之飛行修正控 晋：田 圖。如圖所示，本案之飛行器之飛行修正控制裝 置^=控制-飛行器（圖未示）’該飛行器至少具有—動力機組、 l工②、-接收端及—降落機制，本案之飛行修正控制裝 括：一加速度感測器1〇;—類比/數位轉換器11;一微控制哭12· :=13;以及一參數設定通訊14所組合而成。其；；飛行 為之動力機組、遙控器、接收端及降落機制並非本創作 在此不擬贅述。 ”’又 其t，該加速度感測器10係裝置於該飛行器上其可感測及計 异该飛行器飛行時之加速度。 該類比/數位轉換器（A/D converter)11係耦接至該加速度感測 器10,可將該加速度感測器10所感測之加速度轉換缝位型式。 该微控制器12係為本案之核^ ’其純至該類比/數位轉換器 1,1，可接收經該類比/數位轉換器彳彳轉換後之數位型式加速度資料 並加以計算、處理後傳送至該記憶體13儲存。 ^該記憶體13制馬接至該微控制器12,其可儲#該飛行器之飛 行記錄供該微控制器彳2參考。 该苓數設定通訊介面14係耦接至該微控制器12，可供使用者 6 M290485 設定該飛行器之操作模式或路徑規書彳 例等等模式機制。 如可设疋其啟崎止/比 本創作於運作時’該微控制器12於接收到 值丑^考，玄5己f思體1 3中之飛行記錄而一 控制該動力機組之動力輸出並據以控制参飛:1虎’以 由上述結構之飛行修正控制裝置，確可改盖=…飛行。藉 位置偵測回授而容易導致墜機之缺點。。白知搖控飛行器因不具 此外，本創作之&行修正控制装置進_步包括 =入單元15,其分_接至該加速度感測器， ，器彳2、記憶體13、及參數設定通訊介面14數= 所需之直流電源。 乂仏應/、 此外，本創作之飛行修正控制裝置進—步包括至少—组 :器係柄接至該類比/數位轉換器”，且其數量可視需；二 =，::：_該動力機組之溫度狀態並輸出至該類比/數位轉換： 制成數位型式再輸出至該微㈣器12進行判斷，以供控 k動力機組之動力匹配、警示異常或者自動降落之依據。 ^卜’本創作之飛行修正控制裝置係以一個維度⑼咖 以提供學習飛行或嘗試自動飛航控制之玩家-個馬上可 气介面7位置控制的平台。其控制信號之修正功能除了可透過通 亦C將二維1呈ί修正其啟動’停止/比例等等模式機制之外，其硬體 ^ 維包成―個模組’因其基本單元架構未曾改變。 有下：二述:本創作之飛行修正控制裝置較之習知搖控飛行器具 :下列優點·· i•可以在無遙控動作時自動控制停留原位以避免事 生手拿Γ定上空飛行時控制動作與自動反饋修正之比例，以避免 免:::i3·可伯測過大危險動作，自動反饋修正停留原位，以避 析結構力上限;4.可規劃自動飛行路線;5.可搭配影像分 氚仃控制（如巡戈飛彈）；6可用於車輛自動駕馱控制；7 7 M290485 比赛中G力之紀錄分 主動反饋防震系統控 可用於線性滑軌動作偵測；8·可作為赛車選手 析及缺點改善；9·可用於偵測物體震動以作為 制等功能。 尸η以 、經田本案之實施 發出之屌妒抻士 於接收到遙控器所M290485 VIII. New description: [New technical field] (4) Line correction control device, especially the type-address to control the flight of the aircraft: ❼ 录 录 and turn out the correction control message [previous technology] "... Correction (4) Installation. Press, the general remote control aircraft 'remote control helicopter helmet ^ ^ educational significance' but the entry is quite difficult: because of the science α 彺彺 first to save a lot of money in exchange for lessons. "The flight correction control device of the aircraft has a dimension of::: When receiving the original control signal sent by the remote controller, the value of the G-gens sensed by the acceleration minus the reference can be referred to the memory. The flight record 1 t control signal is used to control the flight of the aircraft to provide a player to learn flight or attempt automatic air navigation control - a platform for stable position control that can be obtained immediately. [New content] The purpose of this creation Providing a flight correction control device for an aircraft, in units of dimensions, when receiving the original control signal sent by the remote controller, based on the sensed sensor The G value is referenced to the flight record in the memory = output correction control signal to control the flight of the aircraft, and to provide a platform for the player to learn the flight control or the automatic flight control of the I. For the above purposes, the flight correction control device of the present aircraft has a power unit, a remote control state, a receiving end and a landing mechanism, and the flight correction control device includes an acceleration sensor. The same can sense and calculate the acceleration of an aircraft when flying; a type of analog/digital converter coupled to the acceleration sensor can convert the acceleration sensed by the acceleration sensor into a digital type; a micro control 5 M290485 The 'coupled to the analog/digital converter, which can be processed; a note I#, coupled with the acceleration of the $H^ vertical type and the body is connected to the phase controller for storing the flight crying ^二和: The communication interface is transferred to the microcontroller, two:::::# for pull or road planning'·俾The microcontroller receives the remote/U value Remembrance The fly number to control the flight of the aircraft. The output-correction control message allows the review board to further understand the structure, features and objectives of the creation, the drawings and the detailed description of the preferred embodiment. [Implementation] [Implementation] σ Please refer to Figure 1, which shows that this is the flight modification of the aircraft of the legislation. Correction control device ^=Control-aircraft (not shown)' The aircraft has at least a power unit, a power station 2, a receiving end and a landing mechanism. The flight correction control of the present case includes: an acceleration sensor 1; - analog/digital converter 11; a micro-control cry 12: :=13; and a parameter setting communication 14 combined; its; flight power unit, remote control, receiving end and landing mechanism are not in this creation This is not intended to be repeated. Further, the acceleration sensor 10 is mounted on the aircraft to sense and account for the acceleration of the aircraft during flight. The analog/digital converter (A/D converter) 11 is coupled to the aircraft. The acceleration sensor 10 can convert the acceleration sensed by the acceleration sensor 10 into a slot type. The microcontroller 12 is a core of the present invention. It is pure to the analog/digital converter 1, and can receive The analog type acceleration data converted by the analog/digital converter is calculated, processed, and transmitted to the memory 13 for storage. ^ The memory 13 is connected to the microcontroller 12, which can store # The flight record of the aircraft is referenced by the microcontroller 彳 2. The parameter setting communication interface 14 is coupled to the microcontroller 12, and the user 6 M290485 can set the operation mode or path specification of the aircraft, etc. Mode mechanism. If it can be set up by Qi Qizhan / than when the creation is in operation, 'the microcontroller 12 receives the value ugly ^ test, Xuan 5 has a flight record in the body 1 3 and controls the power unit The power output and according to the control of the flight: 1 tiger' by the above The flight correction control device can be modified to cover the flight. It can easily lead to the shortcomings of the crash by using the position detection feedback. The Baizhi remote control aircraft does not have the addition, the creation & correction line control device of this creation _ The step includes the input unit 15, which is connected to the acceleration sensor, the device 2, the memory 13, and the parameter setting communication interface 14 = the required DC power supply. 乂仏 Ying /, In addition, the creation The flight correction control device further comprises at least a group: the handle is connected to the analog/digital converter, and the number thereof is as needed; and the second temperature is output to the analogy. /Digital conversion: It is made into a digital type and then output to the micro (four) device 12 for judgment, in order to control the power matching, warning abnormality or automatic landing of the k power unit. ^' The flight correction control device of this creation is a one-dimensional (9) coffee machine to provide players who learn to fly or try automatic flight control - a platform that can be controlled by the air interface 7 position. In addition to the correction function of the control signal, the hardware can be modified into a 'stop/proportion mode mode, and the hardware is packaged into a module. change. There are two: The flight correction control device of this creation is compared with the conventional remote control flight device: the following advantages: · i can automatically control the stop position when there is no remote control action to avoid the fact that when the hand is flying over the sky The ratio of control action and automatic feedback correction is to avoid exemption:::i3·Can be tested for dangerous action, automatic feedback correction stays in place to avoid the upper limit of structural force; 4. Can plan automatic flight route; 5. Can be matched Image bifurcation control (such as patrol missile); 6 can be used for vehicle automatic control; 7 7 M290485 G force record in the game, active feedback, anti-shock system control can be used for linear slide motion detection; 8 · can be used as a match Car player analysis and shortcomings improved; 9· can be used to detect object vibration as a function. The corpse η, the implementation of the tiantian case, the gentleman sent to receive the remote control
號日寸，可根據加速度感測器所感測之加速产G 值=考該記憶體中之飛行記錄而輸出修正控制訊號，以控制：The number of days can be controlled according to the accelerating G value sensed by the acceleration sensor = the flight control record in the memory is output to control the:
Si:二IS”1飛行或#試自動飛航控制之玩家-個馬上 缺點…位置控制的平台，因此，確可解決習知搖控飛行器之 本案所揭示者，乃較佳實施例，舉凡局部 本案之技術思想而為熟習該項技藝之 —1源於 之專利權範疇。 吓㈣推知者，俱不脫本案 ^ ^ ’案無論就目的、手段與功效，在在S貞亍s 習知之技術特徵，且其首先創作合於實用，亦在在於 實感德便。 委貝月察，亚祈早日賜料利，俾嘉惠社會， 【圖式簡單說明】Si: Two IS"1 flight or #trial automatic flight control player - an immediate shortcoming ... position control platform, therefore, it can solve the disclosure of the conventional remote control aircraft, which is a preferred embodiment, The technical idea of this case is to familiarize yourself with the patent right of the craft. 1 Scared (4) Inferred, no matter the case ^ ^ 'Whether the purpose, means and effects, in the technology of S贞亍s Characteristics, and its first creation is practical and practical, and it is also in the sense of real virtue. Weibei Yuecha, Yaqi early to give benefits, 俾嘉惠社会, [Simple diagram]
圖1為一示意圖，其繪示本案一 正控制裝置之方塊示意圖。 【主要元件符號說明】 較佳實施例之飛行 器之飛行修 加速度感測器10 微控制器1 2 參數設定通訊14 溫度感測器16 類比/數位轉換器H 記憶體13 直流電源穩壓輸入單元，5 8BRIEF DESCRIPTION OF THE DRAWINGS Fig. 1 is a schematic view showing a block diagram of a positive control device of the present invention. [Description of main components and symbols] Flight acceleration sensor 10 of the preferred embodiment Microcontroller 1 2 Parameter setting communication 14 Temperature sensor 16 Analog/digital converter H Memory 13 DC power supply voltage stabilization input unit, 5 8