航空电子技术
航空電子技術
항공전자기술
AVIONICS TECHNOLOGY
2014年
2期
1-3,13
,共4页
测距%多普勒频移%递推法%相差定位%无源定位
測距%多普勒頻移%遞推法%相差定位%無源定位
측거%다보륵빈이%체추법%상차정위%무원정위
ranging%Doppler shift%recurrence method%phase difference position%passive location
在机载站飞行方向前方某一距离处的多普勒频移能够通过递推计算的方法由站点当前位置处的相位测量结果而被直接确定。进一步利用频移和角度之间的变换,由多普勒频移的虚拟递推值即可求得载机飞行路线前方虚拟距离处的目标方位,由此就可在机载单站平台上通过三角定位法,实现仅基于相差测量的无源测距。
在機載站飛行方嚮前方某一距離處的多普勒頻移能夠通過遞推計算的方法由站點噹前位置處的相位測量結果而被直接確定。進一步利用頻移和角度之間的變換,由多普勒頻移的虛擬遞推值即可求得載機飛行路線前方虛擬距離處的目標方位,由此就可在機載單站平檯上通過三角定位法,實現僅基于相差測量的無源測距。
재궤재참비행방향전방모일거리처적다보륵빈이능구통과체추계산적방법유참점당전위치처적상위측량결과이피직접학정。진일보이용빈이화각도지간적변환,유다보륵빈이적허의체추치즉가구득재궤비행로선전방허의거리처적목표방위,유차취가재궤재단참평태상통과삼각정위법,실현부기우상차측량적무원측거。
Doppler shift at a certain position in front of the flight direction of airborne station can be directly determined by recurrence method and by making use of the measurement result for phase difference at current position. Furthermore, using transform between Doppler shift and angle, the target's azimuth can be determined by dummy recurrence value of Doppler shift at dummy position in front of the flight direction of airborne station. Therefore, the passive ranging only based on phase difference measuring can be realized by triangle position fixed on single airborne observer platform.