本文選題：襟縫翼 + 嵌入式　； 參考：《北京交通大學》2012年碩士論文

【摘要】：在全人類的發(fā)展歷史中,早在遠古時代,人們就幻想能夠像鳥兒那樣在天空自由的飛翔,馳騁于藍天白云之中。飛機是借助于空氣飛行的的裝置,飛機的襟縫翼便是位于飛機機翼上的一部分可以靈活轉動的裝置,這樣就可以有效的增加飛機機翼的效率。 襟縫翼的控制一般都不是獨立的,而是附屬于飛機的其它控制系統(tǒng),對于襟縫翼的驅動主要是液壓驅動�；蛘呤呛唵蔚碾姎饪刂�。液壓驅動襟翼會出現“剪刀差”現象,使系統(tǒng)復雜化。本文設計的襟縫翼控制系統(tǒng)是基于電機控制的。 本文首先介紹襟縫翼控制系統(tǒng)實現是硬件環(huán)境,應用嵌入式開發(fā),在DSP芯片TMS320F2812上實現,開發(fā)環(huán)境是CCS (Code Composer Studio)。本系統(tǒng)由翼面位置控制器、電機轉速控制器和接口數據處理等構成。襟縫翼控制系統(tǒng)的接口方式應用的是RS422(平衡電壓數字接口電路的電氣特性)標準,系統(tǒng)的輸入數據來自采集編碼設備,經襟縫翼控制系統(tǒng)處理后的數據發(fā)送給驅動解碼設備。 在軟件實現方面,襟縫翼控制系統(tǒng)由C語言開發(fā),軟件系統(tǒng)由上電自檢、10ms定時中斷和RS422接收中斷組成。10ms定時中斷主要用來完成周期任務,比如翼面位置控制器、電機轉速控制器對輸入數據的處理和定期輸出電機的輸入電壓；接收中斷主要用來接收數據,只有當有數據傳入的時候,才會調用相應的接收函數。 本文設計的襟縫翼控制系統(tǒng),就是通過駕駛艙的操作桿,飛行員設置襟翼/縫翼的位置狀態(tài)(位置角度),并通過閉環(huán)反饋控制器控制襟翼和縫翼的運動,使之達到目標狀態(tài)。襟縫翼控制系統(tǒng),對于襟翼或縫翼的控制是相互獨立,且控制原理相同,實現對襟縫翼控制的智能化,并有利于以后對襟縫翼控制系統(tǒng)的擴展,比如當襟縫翼位置確定且長時間不改變時,可以讓CPU騰出時間檢測各個硬件模塊等。 本文的最后,運用mat lab的simulink工具,對本文設計的襟縫翼控制系統(tǒng)進行了仿真,從而來驗證第一部分的理論,通過仿真結果,也可以反饋給第一部分,對第一部分進行修改等。另外,本文還介紹了怎么用mat lab進行數據擬合,這就使得,在實驗條件允許的情況下,可以采集大量的飛機襟縫翼控制系統(tǒng)的相關數據,找出規(guī)律或數學表達式,反過來指導和修改襟縫翼控制系統(tǒng)的相關參數和函數模型。這就使得本文所設計的襟縫翼控制系統(tǒng)具有了一定的實用性。
[Abstract]:In the development history of all mankind, as early as in ancient times, people fantasized that they could fly freely in the sky like birds, galloping in the blue sky and white clouds. Aircraft is the aid of air flight device, the flap-fin is located on the wing of the aircraft part of the device can be flexibly rotated, which can effectively increase the efficiency of the wing of the aircraft. The control of flapflange is not independent, but is attached to other control systems of aircraft. The drive of flapflange is mainly hydraulic drive. Or simple electrical control. Hydraulic-driven flap will appear "scissors difference" phenomenon, making the system complex. The design of the flap-fin control system in this paper is based on the motor control. This paper first introduces the realization of the flap-fin control system is a hardware environment, the application of embedded development, implemented on DSP chip TMS320F2812, the development environment is CCS Code Composer Studio. The system consists of wing position controller, motor speed controller and interface data processing. The interface mode of the slit wing control system is based on the RS422 (Electrical characteristics of balanced Voltage Digital Interface Circuit). The input data of the system come from the acquisition and coding equipment, and the data processed by the slit wing control system is sent to the driver decoding device. In the aspect of software realization, the flap-fin control system is developed by C language. The software system is composed of 10 Ms timing interrupt and 10 Ms RS422 receiving interrupt, which are mainly used to complete periodic tasks, such as wing position controller. The motor speed controller processes the input data and periodically outputs the input voltage of the motor, and the receiving interrupt is mainly used to receive the data, only when the data is passed in, the corresponding receiving function will be called. The flap-fin control system designed in this paper is to set the flap / slit position state (position angle) through the operating lever of the cockpit, and control the flap and slit motion through the closed-loop feedback controller to make it reach the target state. The flapflange control system is independent of each other for flap or slit wing control, and the control principle is the same. It realizes the intelligent control of the flapflange wing, and is conducive to the expansion of the flap-fin control system in the future. For example, when the position of the flapside is determined and not changed for a long time, the CPU can free time to detect the various hardware modules and so on. At the end of this paper, the flap-fin control system designed in this paper is simulated by using the simulink tool of mat lab to verify the theory of the first part. Through the simulation results, it can also be fed back to the first part, and the first part can be modified and so on. In addition, this paper also introduces how to use mat lab to carry out data fitting, which makes it possible to collect a large number of relevant data of aircraft flap-wing control system and find out the law or mathematical expression when the experimental conditions permit. In turn, it guides and modifies the relevant parameters and function models of the flapside control system. This makes the design of the flap-fin control system has a certain practicability.
【學位授予單位】：北京交通大學
【學位級別】：碩士
【學位授予年份】：2012
【分類號】：V227.6;TP273;TP368.1

【參考文獻】

相關期刊論文 前10條

1 于水生;;DSP芯片介紹及其選型[J];單片機與嵌入式系統(tǒng)應用;2006年04期

2 馮元珍;屠小明;羅建平;;MATLAB軟件在曲線擬合中的應用[J];福建電腦;2007年03期

3 范立欽;林國鋒;;機動襟翼在實現直接升力控制中的應用研究[J];飛行力學;1991年04期

4 忻鼎定,余光志,袁禮;大后掠翼大迎角定常與非定常俯仰氣動特性及其控制[J];航空學報;1997年02期

5 高春鳴,黃園媛,陳火旺;基于CCS的軟件規(guī)范描述及實例研究[J];計算機工程與應用;2005年23期

6 嚴少波;黃建國;;飛機后緣襟翼運動同步性設計和計算[J];民用飛機設計與研究;2011年01期

7 黃智偉;幾款通信用DSP芯片簡介[J];世界電子元器件;1999年02期

8 應啟珩;數字信號處理器第二講 實時DSP系統(tǒng)設計開發(fā)流程和DSP處理器開發(fā)工具簡介[J];世界電子元器件;2005年02期

9 付艷茹;;基于MATLAB曲線擬合的應用研究[J];吉林師范大學學報(自然科學版);2010年02期

10 程翔,韓昌彩,袁東風;在初步使用DSP的CCS系統(tǒng)時所遇問題的解答[J];山東電子;2003年02期

相關碩士學位論文 前6條

1 鄭云;自適應機翼構型的選擇方法研究[D];西北工業(yè)大學;2007年

2 張弓;多段翼型縫道流動的相似準則研究[D];西北工業(yè)大學;2007年

3 周傳祥;基于DSP的導航/飛控嵌入式系統(tǒng)設計[D];西北工業(yè)大學;2007年

4 包敦永;民機縫翼機構可靠性若干問題分析與試驗方法研究[D];南京航空航天大學;2008年

5 張巍;基于ARM9的嵌入式汽車導航與防盜系統(tǒng)的設計[D];大連海事大學;2009年

6 王承啟;嵌入式系統(tǒng)設計方法研究與嵌入式避障機器人的實現[D];北京交通大學;2009年

，

本文編號：1951552