Lunar Formation Control Using the Differential Solar Radiation Pressure

被引：0

作者：

Gurfil, Pini ^{[1
]}

Nie, Tao ^{[2
]}

机构：

[1] Technion Israel Inst Technol, Fac Aerosp Engn, IL-32000 Haifa, Israel

[2] Harbin Inst Technol, Res Ctr Satellite Technol, Harbin 150001, Heilongjiang, Peoples R China

来源：

2019 27TH MEDITERRANEAN CONFERENCE ON CONTROL AND AUTOMATION (MED) | 2019年

关键词：

D O I：

10.1109/med.2019.8798528

中图分类号：

TP [自动化技术、计算机技术];

学科分类号：

0812 ;

摘要：

Using differential solar radiation pressure (DSRP) for formation keeping is not new. However, there is no design of a DSRP-based controller for lunar satellite formation keeping, where the C-22 sectorial harmonic and third-body effects are large, other than the J(2) zonal harmonic. This paper develops a DSRP-based controller utilizing mean orbital elements feedback for controlling satellites in a bounded region based on the astrodynamical analysis. It is shown that the most effective way to mitigates the drifts for using SRP is to adjust the semi-major axis. Numerical simulation results illustrate the new DSRP-based controller has the ability to arrest the relative distance drifts for serval years.

引用

页码：221 / 226

页数：6

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