High Precision Computational Method of Two-Way Range-Rate in Long-Distance Deep Space Exploration

JIN Weitong; LI Fei; YANG Xuan; YAN Jianguo; YE Mao; HAO Weifeng; QU Chunkai

doi:10.13203/j.whugis20170020

Volume 43 Issue 10

Oct. 2018

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Geomatics and Information Science of Wuhan University > 2018 > 43(10): 1483-1489. > DOI: 10.13203/j.whugis20170020

JIN Weitong, LI Fei, YANG Xuan, YAN Jianguo, YE Mao, HAO Weifeng, QU Chunkai. High Precision Computational Method of Two-Way Range-Rate in Long-Distance Deep Space Exploration[J]. Geomatics and Information Science of Wuhan University, 2018, 43(10): 1483-1489. DOI: 10.13203/j.whugis20170020

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High Precision Computational Method of Two-Way Range-Rate in Long-Distance Deep Space Exploration

1.
State Key Laboratory of Information Engineering in Surveying, Mapping and Remote Sensing, Wuhan University, Wuhan 430079, China
2.
Chinese Antarctic Center of Surveying and Mapping, Wuhan University, Wuhan 430079, China

Funds:

The National Natural Science Foundation of China 41374024

The National Natural Science Foundation of China 41604004

The National Natural Science Foundation of China 41174019

the Hubei Province Natural Science Foundation Innovation Group Project 2015CFA011

the Open Research Fund of State Key Laboratory of Astronautic Dynamics 2016ADL-DW0103

the Open Research Fund of State Key Laboratory of Space Target Measurement

the China Postdoctoral Science Foundation 2016M602360

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Author Bio:
JIN Weitong, postgraduate, specializes in planetary spacecraft precision orbit determination. E-mail: jwt_whdx@whu.edu.cn
Corresponding author:
YE Mao, PhD. E-mail: mye@whu.edu.cn
Received Date: April 27, 2017
Published Date: October 04, 2018

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Abstract

Abstract

For precise orbit determination of deep space exploration, precision of traditional two-way range-rate model is limited by computers' word length, where the main error source is the simple differenciation of two subsequent Newtonian ranges(up-leg and down-leg) devided by the counting interval. So interplanetary two-way range-rate model is built up in this paper to compute these two necessary differences highy precisely. Of course, we give the formula of this new model and its detailed steps as well as necessary recursion formula of Chebyshev differential polynomial. The new model is implemented in Wuhan University deep-space orbit determination and gravity recovery system-WUDOGS and two scenarios of simulation are adopted to validate it from two aspects:precision of calculation values and initial orbit based on Mars express mission. Simulating results show that the new model can improve precision of calculation values by two orders of magnitude, and reduce extra numerical error during orbit determination, which can provide reference for orbit determination in long-distance deep space exploration of high precision in China.
- deep space exploration,
- precise orbit determination(POD),
- interplanetary two-way range-rate model,
- Chebyshev differential,
- WUDOGS

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References (24)

References

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