Study on Zero Relative Radial Acceleration Region of Formation near Sun-Earth Libration Points under Solar Radiation Pressure

LI Zhenyu1, LI Xiangyu1, QIAO Dong1, HUO Zhuoxi2

PDF(4787 KB)
PDF(4787 KB)
Journal of Deep Space Exploration ›› 2023, Vol. 10 ›› Issue (6) : 631-640. DOI: 10.15982/j.issn.2096-9287.2023.20220112

Study on Zero Relative Radial Acceleration Region of Formation near Sun-Earth Libration Points under Solar Radiation Pressure

  • LI Zhenyu1, LI Xiangyu1, QIAO Dong1, HUO Zhuoxi2
Author information +
History +

Abstract

Formation interferometry near the Sun-Earth libration point is an essential direction for developing high-precision astronomical observation. Keeping the formation configuration stable for a long time is the premise of achieving high-precision measurement. However, the solar radiation pressure will disturb the satellite’s orbit, which challenges the formation configuration’s stability. This paper studies the stable region of formation motion near the libration point under the influence of solar radiation pressure. Based on the Sun-Earth three-body model considering solar radiation pressure, then linearizing the dynamic equation near the reference trajectory of the formation, the analytical expression of the zero relative radial acceleration region near the chief satellite is derived. It is found that the zero relative radial acceleration region is a quadric surface passing through the reference trajectory. The evolution characteristics of zero relative radial acceleration region are further analyzed, and the variation law of region distribution with reference trajectory type, amplitude, and phase is given. Finally, the formation configuration evaluation indexes such as shape, size, and coplanarity are defined. The formation configuration design and control method based on zero relative radial acceleration region is proposed and applied to the design of the five-satellite formation mission. The simulation results show that the formation configuration is bounded within 70 days, and the change rate of the relative distance between the chief satellite and deputy satellite is less than 2% in the first 60 days. In this paper, the study of zero relative radial acceleration region under the influence of solar radiation pressure can provide a basis for designing future Sun-Earth libration point interferometry formation orbits.

Keywords

zero relative radial acceleration region / solar radiation pressure / formation flight / libration point

Cite this article

Download citation ▾
LI Zhenyu, LI Xiangyu, QIAO Dong, HUO Zhuoxi. Study on Zero Relative Radial Acceleration Region of Formation near Sun-Earth Libration Points under Solar Radiation Pressure. Journal of Deep Space Exploration, 2023, 10(6): 631‒640 https://doi.org/10.15982/j.issn.2096-9287.2023.20220112

References

[1] BANNON E T,WEED K,KNIGHT J S,et al. Architectures to reduce heater power for large space telescopes[C]//Proceedings of AIAA SCITECH 2022 Forum. San Diego:AIAA,2022.
[2] PRUSTI T,DE BRUIJNE J H J,BROWN A G A,et al. The GAIA mission[J]. Astronomy & Astrophysics,2016,595:A1.
[3] DOMINGO V,FLECK B,POLAND A I. The SOHO mission:an overview[J]. Solar Physics,1995,162(1):1-37.
[4] FRIDLUND C V M. Darwin-the infrared space interferometry mission[J]. ESA Bulletin,2000,103(3):20-25.
[5] BEICHMAN C A,WOOLF N J,LINDENSMITH C A. The Terrestrial Planet Finder(TPF):a NASA origins program to search for habitable planets[M]. Washington,DC:National Aeronautics and Space Administration,1999.
[6] 安然,王敏,梁新刚. 基于不变流形的地-月L2点转移轨道优化设计[J]. 深空探测学报(中英文),2017,4(3):252-257.
AN R,WANG M,LIANG X G. Transfer trajectory optimal design for Earth-Moon L2 based on invariant manifolds[J]. Journal of Deep Space Exploration,2017,4(3):252-257.
[7] 乔栋,黄江川,崔平远,等. 嫦娥二号卫星飞越Toutatis小行星转移轨道设计[J]. 中国科学:技术科学,2013,43(5):487-492.
QIAO D,HUANG J C,CUI P Y,et al. Transfer orbit design of Chang'e-2 satellite overflight Toutatis asteroid[J]. Scientia Sinica(Technologica),2013,43(5):487-492.
[8] BARDEN B T,HOWELL K C. Fundamental motions near collinear libration points and their transitions[J]. The Journal of the Astronautical Sciences,1998,46(4):361-378.
[9] HOWELL K C,MARCHAND B G. Natural and non-natural spacecraft formations near the L1 and L2 libration points in the Sun-Earth/Moon ephemeris system[J]. Dynamical Systems,2005,20(1):149-173.
[10] GOMEZ G,MARCOTE M,MASDEMONT J J,et al. Zero relative radial acceleration cones and controlled motions suitable for formation flying[J]. The Journal of the Astronautical Sciences,2005,53(4):413-431.
[11] HÉRITIER A,HOWELL K C. Natural regions near the Sun-Earth libration points suitable for space observations with large formations[J]. The Journal of the Astronautical Sciences,2011,60:87-108.
[12] HÉRITIER A,HOWELL K C. Dynamical evolution of natural formations in libration point orbits in a multi-body regime[J]. Acta Astronautic,2014,102:332-340.
[13] SALAZAR F J T,MASDEMONT J J,GÓMEZ G,et al. Zero,minimum and maximum relative radial acceleration for planar formation flight dynamics near triangular libration points in the Earth–Moon system[J]. Advances in Space Research,2014,54(9):1838-1857.
[14] SALAZAR F J T,WINTER O C,MACAU E E,et al. Zero drift regions and control strategies to keep satellite in formation around triangular libration point in the restricted Sun-Earth-Moon scenario[J]. Advances in Space Research,2015,56(7):1502-1518.
[15] SALAZAR F J T,WINTER O C,MAACU E E,et al. Natural formations at the Earth-Moon triangular point in perturbed restricted problems[J]. Advances in Space Research,2015,56(1):144-162.
[16] KUTLU A,TEKINALP O. Formation flight design near Sun-Earth collinear libration points under the effect of disturbances[C]//Proceedings of 2019 9th International Conference on Recent Advances in Space Technologies(RAST). Istanbul:IEEE,2019.
[17] FARQUHAR R W. The control and use of libration-point satellites[M]. Stanford:Stanford University,1969.
[18] LI H,WILLIAMS T. Formation design and control with solar radiation pressure for translunar libration point[J]. Advances in the Astronautical Sciences,2006,123:1427-1446.
[19] GORDON S C. Orbit determination error analysis and station-keeping for libration point trajectories[D]. West Lafayette:Purdue University,1991.
[20] FERRARI F,LAVAGNA M. Suitable configurations for triangular formation flying about collinear libration points under the circular and elliptic restricted three-body problems[J]. Acta Astronautica,2018,147:374-382.
PDF(4787 KB)

Accesses

Citations

Detail

Sections
Recommended

/