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旋转环境下的无线时钟抖动估计与修正方法
2022年电子技术应用第8期
卢翔宇1,陈正武1,刘 雄2
1.中国空气动力研究与发展中心 气动噪声控制实验室,四川 绵阳621000; 2.西南科技大学 信息工程学院,四川 绵阳621000
摘要: 直升机旋翼表面非定常载荷测量试验中,导电滑环的性能优劣和现场环境的电磁辐射对外部时钟信号的质量影响较大,受影响的外部时钟信号会导致错误的采集动作,从而无法准确地获取特定方位角处的载荷数据。为提高外部时钟信号的品质,提出一种用于旋转环境下的数据采集系统的无线时钟抖动估计及修正方法,即外部时钟信号经无线收发模块传输,采用两组相位差90°的三角波进行等幅度斜边估计时钟抖动量,并且使用拉格朗日插值算法修正传感器的采样值。仿真与风洞表明,该方法能有效地减小外部时钟抖动造成的采集误差,对准确测量旋转环境下旋翼表面的载荷信号具有显著效果。
中圖分類(lèi)號(hào): TN919.3
文獻(xiàn)標(biāo)識(shí)碼: A
DOI:10.16157/j.issn.0258-7998.212498
中文引用格式: 盧翔宇,陳正武,劉雄. 旋轉(zhuǎn)環(huán)境下的無(wú)線(xiàn)時(shí)鐘抖動(dòng)估計(jì)與修正方法[J].電子技術(shù)應(yīng)用,2022,48(8):76-80,85.
英文引用格式: Lu Xiangyu,Chen Zhengwu,Liu Xiong. Wireless clock jitter estimation and correction method in rotating environment[J]. Application of Electronic Technique,2022,48(8):76-80,85.
Wireless clock jitter estimation and correction method in rotating environment
Lu Xiangyu1,Chen Zhengwu1,Liu Xiong2
1.Laboratory of Aerodynamic Noise Control,China Aerodynamic Research and Development Center,Mianyang 621000,China; 2.School of Information Engineering,Southwest University of Science and Technology,Mianyang 621000,China
Abstract: In the measurement test of unsteady load on helicopter rotor surface, the performance of slip ring and the electromagnetic radiation of the field environment have great influence on the quality of external clock signal. In some serious cases, the affected external clock signal may lead to erroneous acquisition actions, which makes it impossible to accurately obtain the load data at a specific azimuth. In order to improve the quality of the external clock signal, a wireless clock jitter estimation and correction method of data acquisition system in rotating environment is proposed. The external clock signal is transmitted through the wireless transceiver modules, two sets of triangular waves with the phase difference of 90° are used to estimate the clock jitter with equal amplitude hypotenuse, and the Lagrange interpolation algorithm is used to correct the samples of sensors. Simulation and wind tunnel tests show that this method can effectively reduce the acquisition error caused by external clock jitter, and has significant effect on accurately measuring the load signal on the rotor surface in rotating environment.
Key words : external clock;clock jitter;data acquisition system;triangle wave;interpolation correction

0 引言

    在直升機(jī)旋翼槳葉表面非定常載荷測(cè)量試驗(yàn)中,需要準(zhǔn)確測(cè)量槳葉旋轉(zhuǎn)過(guò)程中其表面載荷的變化規(guī)律,即采集不同方位角時(shí)對(duì)應(yīng)的壓力信號(hào)[1]。使用與槳葉同步旋轉(zhuǎn)的編碼器的輸出脈沖作為數(shù)據(jù)采集的外部時(shí)鐘信號(hào),可以準(zhǔn)確提供槳葉的方位角信息[2-6]。目前通常采用有線(xiàn)的方式將時(shí)鐘信號(hào)進(jìn)行傳送:即通過(guò)導(dǎo)電滑環(huán)和線(xiàn)纜將編碼器脈沖信號(hào)輸送至數(shù)據(jù)采集設(shè)備。試驗(yàn)中發(fā)現(xiàn),外部時(shí)鐘信號(hào)經(jīng)過(guò)干擾環(huán)境下的長(zhǎng)距離傳輸和導(dǎo)電滑環(huán)后,其信號(hào)質(zhì)量會(huì)受到影響[7],尤其在導(dǎo)電滑環(huán)磨損后以及時(shí)鐘信號(hào)線(xiàn)與動(dòng)力強(qiáng)電線(xiàn)纜長(zhǎng)距離并行部署等重干擾情況下,時(shí)鐘信號(hào)會(huì)出現(xiàn)高頻毛刺和變形,導(dǎo)致數(shù)據(jù)采集設(shè)備產(chǎn)生錯(cuò)誤的采集動(dòng)作,從而無(wú)法實(shí)現(xiàn)相同相位的等角度采集。




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作者信息:

盧翔宇1,陳正武1,劉  雄2

(1.中國(guó)空氣動(dòng)力研究與發(fā)展中心 氣動(dòng)噪聲控制實(shí)驗(yàn)室,四川 綿陽(yáng)621000;

2.西南科技大學(xué) 信息工程學(xué)院,四川 綿陽(yáng)621000)




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