An overview of the laser ranging method of space laser altimeter

被引:24
|
作者
Zhou, Hui [1 ,2 ]
Chen, Yuwei [2 ]
Hyyppa, Juha [2 ]
Li, Song [1 ]
机构
[1] Wuhan Univ, Elect Informat Sch, Luojia Hill, Wuhan 430072, Hubei, Peoples R China
[2] Finnish Geospatial Res Inst, Dept Remote Sensing & Photogrammetry, Geodeerinne 2, Masala 02430, Finland
基金
芬兰科学院;
关键词
Space laser altimeter; Ranging method; Leading edge timing; Constant fraction discrimination; Waveform processing and analyzing; Photon counting timing; NORTHERN-HEMISPHERE; PERFORMANCE; TOPOGRAPHY; INSTRUMENT; MISSION; MERCURY; MARS; MODEL; SHAPE; CHANGE-1;
D O I
10.1016/j.infrared.2017.09.011
中图分类号
TH7 [仪器、仪表];
学科分类号
0804 ; 080401 ; 081102 ;
摘要
Space laser altimeter is an active remote sensing instrument to measure topographic map of Earth, Moon and planetary. The space laser altimeter determines the range between the instrument and laser footprint by measuring round trip time of laser pulse. The return pulse reflected from ground surface is gathered by the receiver of space laser altimeter, the pulsewidth and amplitude of which are changeable with the variability of the ground relief. Meantime, several kinds of noise overlapped on the return pulse signal affect its signal-to-noise ratio. To eliminate the influence of these factors that cause range walk and range uncertainty, the reliable laser ranging methods need to be implemented to obtain high-precision range results. Based on typical space laser altimeters in the past few decades, various ranging methods are expounded in detail according to the operational principle of instruments and timing method. By illustrating the concrete procedure of determining time of flight of laser pulse, this overview provides the comparison of the employed technologies in previous and undergoing research programs and prospect innovative technology for space laser altimeters in future. (C) 2017 Elsevier B.V. All rights reserved.
引用
收藏
页码:147 / 158
页数:12
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