航空兵器
航空兵器
항공병기
HANGKONG BINGQI
2015年
3期
13-17
,共5页
吴振钿%吴发林%付勇%赵剡%钟海波
吳振鈿%吳髮林%付勇%趙剡%鐘海波
오진전%오발림%부용%조섬%종해파
GPS失效%多传感器%组合导航%卡尔曼滤波
GPS失效%多傳感器%組閤導航%卡爾曼濾波
GPS실효%다전감기%조합도항%잡이만려파
GPS-denied%multi-sensors%integrated navigation%Kalman filtering
针对GPS/SINS组合导航系统在GPS间歇性失效环境下导航精度迅速下降的问题,设计了一种低成本的多传感器组合导航系统。该系统由陀螺仪、加速度计、气压计、磁力计和GPS组成,通过卡尔曼滤波器进行信息融合来实现精确的导航定位。针对GPS间歇性失效环境,利用气压计和磁力计的测量信息来辅助SINS进行导航。采用内置MEMS多传感器的智能产品对设计的系统进行了实验验证。实验结果表明,该系统可以在GPS间歇性失效的环境下实现精确的导航定位。
針對GPS/SINS組閤導航繫統在GPS間歇性失效環境下導航精度迅速下降的問題,設計瞭一種低成本的多傳感器組閤導航繫統。該繫統由陀螺儀、加速度計、氣壓計、磁力計和GPS組成,通過卡爾曼濾波器進行信息融閤來實現精確的導航定位。針對GPS間歇性失效環境,利用氣壓計和磁力計的測量信息來輔助SINS進行導航。採用內置MEMS多傳感器的智能產品對設計的繫統進行瞭實驗驗證。實驗結果錶明,該繫統可以在GPS間歇性失效的環境下實現精確的導航定位。
침대GPS/SINS조합도항계통재GPS간헐성실효배경하도항정도신속하강적문제,설계료일충저성본적다전감기조합도항계통。해계통유타라의、가속도계、기압계、자력계화GPS조성,통과잡이만려파기진행신식융합래실현정학적도항정위。침대GPS간헐성실효배경,이용기압계화자력계적측량신식래보조SINS진행도항。채용내치MEMS다전감기적지능산품대설계적계통진행료실험험증。실험결과표명,해계통가이재GPS간헐성실효적배경하실현정학적도항정위。
For the problem that the navigation precision of GPS/SINS integrated navigation declines rapidly under intermittent GPS-denied environment, a low-cost multi-sensor integrated navigation system is designed.The system consists of gyroscope, accelerometer, barometer, magnetometer and GPS, and a-chieves the purpose of accurate navigation and positioning by using Kalman filter for information fusion. For the intermittent GPS-denied environments, the system uses the measurement information of barometer and magnetometer to assist SINS’ s navigation.This system is verified by using smart product with built-in MEMS multiple sensors.The experimental results show that the integrated navigation system can realize precise navigation and positioning under intermittent GPS-denied environment.