由于探测距离远,火星探测任务对干涉测量具有很强的精度需求。首先描述了相位参考甚长基线干涉测量(Very Long Baseline Interferometry,VLBI)原理,介绍了弧段内干涉相时延解模糊方法,阐述了弧段之间相互参考解算干涉相时延流程,给出了...由于探测距离远,火星探测任务对干涉测量具有很强的精度需求。首先描述了相位参考甚长基线干涉测量(Very Long Baseline Interferometry,VLBI)原理,介绍了弧段内干涉相时延解模糊方法,阐述了弧段之间相互参考解算干涉相时延流程,给出了测量误差分析,并利用中国佳木斯深空站、喀什深空站针对射电源对1633+38和1641+399开展了相位参考VLBI试验验证。结果表明,消除模糊度后,相位参考时延精度优于0.1ns。这为提高中国未来深空探测器角位置精度提供一种可行的技术途径。展开更多
To determine the feasibility and practicability of interrupt continuous wave (CW) approach proposed for real time simulating radar intermediate frequency(IF) video signal, theoretical analysis and computer simulation...To determine the feasibility and practicability of interrupt continuous wave (CW) approach proposed for real time simulating radar intermediate frequency(IF) video signal, theoretical analysis and computer simulation were used. Phases at two linked points between the end and beginning of adjoined frames are always consistent; the bias Doppler frequency for the time delay of A/D sampling start responds to that for target acceleration. No digital phase compensation is required at continuous points, and the interrupt CW approach has apparently practical values.展开更多
文摘由于探测距离远,火星探测任务对干涉测量具有很强的精度需求。首先描述了相位参考甚长基线干涉测量(Very Long Baseline Interferometry,VLBI)原理,介绍了弧段内干涉相时延解模糊方法,阐述了弧段之间相互参考解算干涉相时延流程,给出了测量误差分析,并利用中国佳木斯深空站、喀什深空站针对射电源对1633+38和1641+399开展了相位参考VLBI试验验证。结果表明,消除模糊度后,相位参考时延精度优于0.1ns。这为提高中国未来深空探测器角位置精度提供一种可行的技术途径。
文摘To determine the feasibility and practicability of interrupt continuous wave (CW) approach proposed for real time simulating radar intermediate frequency(IF) video signal, theoretical analysis and computer simulation were used. Phases at two linked points between the end and beginning of adjoined frames are always consistent; the bias Doppler frequency for the time delay of A/D sampling start responds to that for target acceleration. No digital phase compensation is required at continuous points, and the interrupt CW approach has apparently practical values.
