Hardware development and measurements of solar Doppler shift for spacecraft orbit determination

被引：0
|
作者：
Henderson, TA [1 ]
Pollock, TC [1 ]
Sinclair, AJ [1 ]
Theisinger, JE [1 ]
Hurtado, JE [1 ]
Junkins, JL [1 ]
机构：
[1] Texas A&M Univ, Dept Aerosp Engn, College Stn, TX 77843 USA
来源：
ASTRODYNAMICS 2003, PTS 1-3 | 2003年 / 116卷
关键词：
D O I：
暂无
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
Autonomous spacecraft navigation throughout our solar system (or wherever the Sun is the dominant visible body) can in theory be achieved by using the Sun as a navigation reference body. This allows a self-contained navigation system to guide a spacecraft into any orbit in the solar system, with no need for ground support. One key to developing such a system is knowledge of the radial velocity of the spacecraft relative to the Sun. Current methods for taking the measurement are discussed in detail and current laboratory results are presented. Future research and the orbit determination algorithm will be included.
引用
收藏
页码：1765 / 1778
页数：14
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