航空感應(yīng)線圈位姿數(shù)據(jù)采集系統(tǒng)研發(fā)
[Abstract]:In the measurement flight of fixed wing time domain aeronautical electromagnetic exploration system, the attitude of three component induction coil sensor changes and vibrates with the swing of pods, and its attitude change and vibration have a great influence on the measurement performance of fixed wing time domain aeromembrane system. Based on the national 863 project "practical application of fixed wing time domain aeronautical electromagnetic system", the receiving pod of domestic fixed wing time domain aeronautical electromagnetic exploration system and the pose data acquisition system of internal aeronautical induction coil are studied in this paper. This paper mainly completes the position and pose data acquisition and collection of the three-component induction coil suspended on the special star structure vibration avoidance device in the pods and pods during flight, completes the analysis of the motion attitude data of the three-component induction coil, and solves the parameters such as the attitude change law and vibration of the three-component induction coil. It is used to correct the exploration system data and improve the accuracy of the exploration system data, so as to improve the exploration performance of the system. In order to solve the problem that the small space of receiving pod and the condition of battery power supply are limited, and the large and high energy consumption attitude measuring instrument can not be used, a design scheme of small and low power object motion attitude detection and collection system based on embedded processor is proposed. The design selects STM32 embedded processor to transplant FATFS file system to write SD card, completes the collection function of attitude data and GPS data, and uses computer to solve and analyze the attitude data. The original attitude data is transformed and parsed by the data preprocessing software written by LABVIEW software, the attitude data is smoothed and de-noised by Savitzky-Golay filter, and the attitude data is solved by quaternion algorithm. The above process realizes the collection and processing of the moving attitude data of the object, and completes the analysis of the data through the time domain analysis and the frequency domain analysis. Finally, a set of pose data acquisition system, which includes hardware acquisition and software processing, is designed and successfully applied to the measurement flight of aeronautical electromagnetic exploration system in fixed wing time domain. the system works stably and collects a large number of attitude data. Through the analysis of the data, the data feedback of the pod damping device is finally realized.
【學(xué)位授予單位】:北華航天工業(yè)學(xué)院
【學(xué)位級(jí)別】:碩士
【學(xué)位授予年份】:2017
【分類號(hào)】:TP274.2
【參考文獻(xiàn)】
相關(guān)期刊論文 前8條
1 蔣鈺;諶海云;岑汝平;;基于四元數(shù)的四旋翼飛行器姿態(tài)解算算法[J];制造業(yè)自動(dòng)化;2015年23期
2 朱紅運(yùn);王長(zhǎng)龍;王建斌;馬曉琳;;基于奇異值分解和Savitzky-Golay濾波器的信號(hào)降噪方法[J];計(jì)算機(jī)應(yīng)用;2015年10期
3 尹劍;陳紅;楊萌;黃皓;;捷聯(lián)姿態(tài)計(jì)算中方向余弦與四元數(shù)法分析比較[J];四川兵工學(xué)報(bào);2015年09期
4 余芳芳;郭來(lái)功;李良光;;基于STM32F407的微震信息采集系統(tǒng)設(shè)計(jì)[J];工礦自動(dòng)化;2014年07期
5 王琦;林君;于生寶;李冰冰;朱凱光;;固定翼航空電磁系統(tǒng)的線圈姿態(tài)及吊艙擺動(dòng)影響研究與校正[J];地球物理學(xué)報(bào);2013年11期
6 肖敏;劉宇紅;;SD卡硬件加密在工業(yè)MP3中的實(shí)現(xiàn)[J];通信技術(shù);2012年11期
7 趙翔;杜普選;李虎;楊浩淼;;基于MEMS加速度計(jì)和陀螺儀的姿態(tài)檢測(cè)系統(tǒng)[J];鐵路計(jì)算機(jī)應(yīng)用;2012年03期
8 胡平;李文杰;李軍峰;孟慶敏;王緒本;陳曉東;劉瑩瑩;;固定翼時(shí)間域航空電磁勘查系統(tǒng)研發(fā)進(jìn)展[J];地球?qū)W報(bào);2012年01期
,本文編號(hào):2503742
本文鏈接:http://www.sikaile.net/kejilunwen/zidonghuakongzhilunwen/2503742.html