弹箭与制导学报
彈箭與製導學報
탄전여제도학보
JOURNAL OF PROJECTILES, ROCKETS, MISSILES AND GUIDANCE
2015年
2期
163-165
,共3页
黄坤%田晓丽%王瑞华%白敦卓%马迎辉%冯冰玉
黃坤%田曉麗%王瑞華%白敦卓%馬迎輝%馮冰玉
황곤%전효려%왕서화%백돈탁%마영휘%풍빙옥
弹箭%地磁%时变误差%校正
彈箭%地磁%時變誤差%校正
탄전%지자%시변오차%교정
ball%magnetometer%time-varying bias%revise
在弹箭设计过程中,为了获得弹体飞行时的气动参数,通常采用地磁传感器来测量弹体的姿态信息,而采用的三轴磁传感器都存在误差,因此,对误差的校正就显得很有必要了。在文中提出了一种新的校正方法,该方法是对已有的常规误差校正方法的扩展,使之能用来对磁传感器的时变误差进行校正。这种方法可用于复杂电磁环境中的弹载测量系统,可以有效校正磁传感器的测量误差,最后通过仿真实验数据对结果进行了验证。
在彈箭設計過程中,為瞭穫得彈體飛行時的氣動參數,通常採用地磁傳感器來測量彈體的姿態信息,而採用的三軸磁傳感器都存在誤差,因此,對誤差的校正就顯得很有必要瞭。在文中提齣瞭一種新的校正方法,該方法是對已有的常規誤差校正方法的擴展,使之能用來對磁傳感器的時變誤差進行校正。這種方法可用于複雜電磁環境中的彈載測量繫統,可以有效校正磁傳感器的測量誤差,最後通過倣真實驗數據對結果進行瞭驗證。
재탄전설계과정중,위료획득탄체비행시적기동삼수,통상채용지자전감기래측량탄체적자태신식,이채용적삼축자전감기도존재오차,인차,대오차적교정취현득흔유필요료。재문중제출료일충신적교정방법,해방법시대이유적상규오차교정방법적확전,사지능용래대자전감기적시변오차진행교정。저충방법가용우복잡전자배경중적탄재측량계통,가이유효교정자전감기적측량오차,최후통과방진실험수거대결과진행료험증。
In missiles design process, in order to obtain the dynamic parameters of the missile in flight. We usually use the geomagnetic sensor to measure the attitude information of the projectile. However, there are some errors of three-axis magnetometers which we commonly used. Therefore, the calibration of magnetometers measuring error is seems very important. This article put forward a new method which to calibration the time-varying error of three-axis magnetometers. This method is an expansion for the existing method which is constant error. So that the magnetometer can be used for calibration with time-varying bias. This method is particularly suitable for complex electromagnet-ic environment onboard measurement system that can effectively calibration the measure error of three axis magnetometer. Finally, the re-sults were verified by simulation data.