舰船电子对抗
艦船電子對抗
함선전자대항
JIANGCHUAN DIANZI DUIKANG
2012年
2期
62-65
,共4页
弹载%电子侦察系统%坐标变换
彈載%電子偵察繫統%坐標變換
탄재%전자정찰계통%좌표변환
missile-borne%electronic support measure system%coordinate conversion
研究了基于弹载电子侦察（ESM）系统的测量方位与弹体空间三维坐标关系及变换原理，并根据测量方位与弹体姿态信息的解耦关系，得出目标相对于坐标原点的坐标及方位角和俯仰角。仿真结果表明，该方法可用于导引头侦察系统中目标方位的解算及定位。
研究瞭基于彈載電子偵察（ESM）繫統的測量方位與彈體空間三維坐標關繫及變換原理，併根據測量方位與彈體姿態信息的解耦關繫，得齣目標相對于坐標原點的坐標及方位角和俯仰角。倣真結果錶明，該方法可用于導引頭偵察繫統中目標方位的解算及定位。
연구료기우탄재전자정찰（ESM）계통적측량방위여탄체공간삼유좌표관계급변환원리，병근거측량방위여탄체자태신식적해우관계，득출목표상대우좌표원점적좌표급방위각화부앙각。방진결과표명，해방법가용우도인두정찰계통중목표방위적해산급정위。
This paper studies the relationship and conversion principle between the measured directions based on missile-borne electronic support measure （ESM） system and missile-body space 3-D coordinate, deduces the target coordinate relative to the coordinate origin and azimuth, elevation ac- cording to the decoupling relationship between the measured direction and missile-body attitude information. The simulation results show that the method can be used for calculation and position of target direction in seeker reconnaissance system.
