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Research on Modeling Method of Gravitational Field for Binary Asteroid System
- BU Shichao1, WANG Yukai1,2, LI Wendan1, LI Shuang1, NIU Shengda3
Author information
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1. Laboratory of Space New Technology,Nanjing University of Aeronautics and Astronautics,Nanjing 210016,China;
2. Shanghai Engineering Center for Microsatellites,Shanghai 201210,China;
3. Shanghai Institute of Satellite Engineering,Shanghai 201109,China
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History
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Received |
Revised |
13 Apr 2017 |
27 May 2017 |
Issue Date |
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20 May 2022 |
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In this paper, the sphere-sphere model, the ellipsoid-sphere model and the improved restrictive ellipsoid-ellipsoid model are adopted for the gravitational field modeling of the weak gravitational binary asteroid system, and the corresponding complexity and accuracy of the three models increase gradually. The elliptic integral model and the second degree second order spherical harmonic function (which has high calculation efficiency and no integrals) model are adopted to calculate the gravitational potential energy, respectively. The dynamical model of the restricted full three-body problem consisting of binary asteroid system and spacecraft is accurately described. The different gravitational field models of the binary asteroid system 1999KW4 are simulated. And the surfaces of potential energy function and zero velocity curves under different models are given respectively. The coordinate deviations of libration point under different models are compared. The results show that the ellipsoid-ellipsoid model calculated by the second degree second order spherical harmonic function has the advantages of high precision, low complexity, less calculation, higher computing speed, and can accurately model the gravitational field of the binary asteroid system.
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References
[1] Pravec P,Harris A W. Binary asteroid population:1. angular momentum content [J]. Icarus,2007,190(1):250-259
[2] Scheeres D J,Ostro S J,Hudson R S,et al. Orbits close to asteroid 4769 Castalia [J]. Icarus,1996,121:67-87
[3] Scheeres D J,Ostro S J,Hudson R S,et al. Dynamics of orbits close to asteroid 4179 Toutatis [J]. Icarus,1998,132:53-79
[4] Bellerose J,Scheeres D J. Stability of equilibrium points in the restricted full three body problem[J]. Acta Astronautica,2007,60:141-152
[5] Fahnestock E G,Scheeres D J. Simulation of the full two rigid body problem using polyhedral mutual potential and potential derivatives approach [J]. Celestial Mechanics and Dynamical Astronomy,2006,96:317-339
[6] Fahnestock E G,Lee T,Leok M,et al. Polyhedral potential and variational integrator computation of the full two body problem[C]//The 2006 AIAA/AAS Astrodynamics Specialist Meeting.[S.l.]:AIAA,2006.
[7] 李翔宇,乔栋,崔平远. 双体小行星1996FG3捕获与逃逸轨道设计[C]//上海航天技术研究院第二届小行星探测学术研讨论文集.上海:上海航天技术研究院,2014.
Li X Y,Qiao D,Cui P Y. The capture and escape trajectory design of the binary asteroid 1996FG3 [C]// The 2nd Shanghai Academy of Spaceflight Technology Asteroid Exploration Conference. Shanghai:Shanghai Academy of spaceflight Technology,2014.
[8] Bellerose J,Scheeres D J. Restricted full three-body problem:application to binary system 1999 KW4 [J]. Journal of Guidance,Control,and Dynamics,2008,31(1):162-171
[9] Bellerose J. The restricted full three body problem:applications to binary asteroid exploration[D]. Ann Arbor:University OF Michigan,2008.
[10] Kaula W M. Theory of satellite geodesy:applications of satellites to geodesy [M]. Mineola:Dover publications,2000:4-8.
[11] Hu W. Orbital motion in uniformly rotating second degree and order gravity fields [D]. Ann Arbor:the University of Michigan,2002.
[12] Hu W,Scheeres D J. Numerical determination of stability regions for orbital motion in uniformly rotating second degree and order gravity fields [J]. Planetary and Space Science,2004,52(8):685-692