海军航空工程学院学报
海軍航空工程學院學報
해군항공공정학원학보
JOURNAL OF NAVAL AERONAUTICAL ENGINEERING INSTITUTE
2014年
1期
14-18
,共5页
单观测站%机载%运动辐射源%无源定位%修正增益卡尔曼滤波算法
單觀測站%機載%運動輻射源%無源定位%脩正增益卡爾曼濾波算法
단관측참%궤재%운동복사원%무원정위%수정증익잡이만려파산법
single observer%airborne%moving emitter%passive location%MGEKF
针对无源定位系统中,机载单站相对于运动辐射源目标作为状态模型,在测方位角及其变化率基础上,引入多普勒频率变化率参数构建观测模型。常用的扩展卡尔曼滤波(EKF)存在不稳定和精度低的问题,采用修正增益的扩展卡尔曼滤波算法(MGEKF),找出修正函数矩阵,实现定位状态滤波估计。仿真结果表明,MGEKF算法较之EKF算法有较高的定位精度和较快的收敛速度。
針對無源定位繫統中,機載單站相對于運動輻射源目標作為狀態模型,在測方位角及其變化率基礎上,引入多普勒頻率變化率參數構建觀測模型。常用的擴展卡爾曼濾波(EKF)存在不穩定和精度低的問題,採用脩正增益的擴展卡爾曼濾波算法(MGEKF),找齣脩正函數矩陣,實現定位狀態濾波估計。倣真結果錶明,MGEKF算法較之EKF算法有較高的定位精度和較快的收斂速度。
침대무원정위계통중,궤재단참상대우운동복사원목표작위상태모형,재측방위각급기변화솔기출상,인입다보륵빈솔변화솔삼수구건관측모형。상용적확전잡이만려파(EKF)존재불은정화정도저적문제,채용수정증익적확전잡이만려파산법(MGEKF),조출수정함수구진,실현정위상태려파고계。방진결과표명,MGEKF산법교지EKF산법유교고적정위정도화교쾌적수렴속도。
In passive location system, the state model was set up as a airborne single observer moving emitter. The observa-tion model was formed on the base of measuring azimuth angle and its changing rate, and the parameter of Doppler frequen-cy changing rate was introduced. On counter of the instability and low precision in the passive location system with the fre-quently-used“Extended Kalman Filter”(EKF),“modified function matrix”was calculated, and“Modified Gain EKF”(MGEKF)was adopted. The result of simulation indicated that its precision was higher and its convergence speed was fast-er.