Duration of Radar Observation of Space Debris

被引：0
|
作者：
Gavrilov K.Y. [1 ]
Kirdyashkin V.V. [1 ]
Shiryaev V.A. [1 ]
机构：
[1] Moscow Aviation Institute, Moscow
来源：
Russian Engineering Research | 2022年 / 42卷 / Suppl 1期
关键词：
duration; geocentric equatorial coordinate system; radar observations; space debris; spatial objects;
D O I：
10.3103/S1068798X23010082
中图分类号：
学科分类号：
摘要：
Abstract: A new method is proposed for calculating the duration of radar observation of spatial objects. This method is based on kinematic description of the object’s motion; and calculation of the scalar product of the object’s position vector and the vector of the observation point on the Earth’s surface. Sample calculations are presented for the radar visibility of objects on different trajectories. This method may be used to optimize the location of radar stations on the Earth’s surface so as to permit uninterrupted detection and observation of objects in low orbits. © 2022, Allerton Press, Inc.
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页码：S117 / S120
页数：3
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