Abstract
In the design and performance evaluation of a navigation system, the orbit dynamics model, attitude kinematics model, and environment model should be established. This chapter first addresses orbital perturbation model, establishes orbit dynamic equations, and then elaborates on four typical parametric forms for attitude description, the conversion relations between attitude parameters, and the attitude kinematics model corresponding to each parameter. Finally, Mars and asteroids are taken as examples to introduce the modeling methods of celestial environment, including celestial body shape modeling and gravitational field modeling.
This is a preview of subscription content, log in via an institution to check access.
Access this chapter
Tax calculation will be finalised at checkout
Purchases are for personal use only
References
Roman, G., and B. Jean-Pierre. 2001. Ellipsoidal harmonic expansions of the gravitational potential: Theory and application. Celestial Mechanics & Dynamical Astronomy 79 (4): 235–275.
Casotto, S., and S. Musotto. 2013. Methods for computing the potential of an irregular, homogeneous, solid body and its gradient. In Astrodynamics specialist conference, 82–96.
Park, R.S., R.A. Werner, and S. Bhaskaran. 2010. Estimating small-body gravity field from shape model and navigation data. Journal of Guidance, Control and Dynamics 33 (1): 212–221.
Zhang, Renwei. 1998. Attitude dynamics and control of satellite orbit. Beijing: Beihang University Press.
Lu, Zhenduo, and Yongjun Lei. 2013. Satellite attitude measurement and determination. Beijing: National Defense Industry Press.
Xu, Qing, Xun Geng, Chaozhen Lan, et al. 2014. Review of mars topographic mapping. Journal of Deep Space Exploration 1 (1): 28–35.
Konopliv, A.S., and W.L. Sjogren (1995) The JPL Mars gravity field, Mars50c, based upon Viking and Mariner 9 Doppler tracking data. NASA STI/RECON Technical Report N.
Lemoine, F.G., D.E. Smith, D.D. Rowlands, et al. 2001. An improved solution of the gravity field of Mars (GMM-2B) from Mars global surveyor. Journal of Geophysical Research: Planets 106 (E10): 23359–23376.
Konopliv, A.S., R.S. Park, and W.M. Folkner. 2016. An improved JPL Mars gravity field and orientation from Mars orbiter and lander tracking data. Icarus 274: 253–260.
Li, Junfeng, Hexi Baoyin, and Fanghua Jiang. 2014. Dynamics and control of interplanetary flight. Beijing: Tsinghua University Press.
Cui, Hutao, Zhenjiang Zhang, and Meng Yu. 2012. Computing and analysis of gravity field of Eros433 using polyhedron model. Journal of Haerbin Institute of Technology 44 (3): 17–22.
Richardson, D.C., Z.M. Leinhardt, H.J. Melosh, et al. 2002. Gravitational aggregates: evidence and evolution. In Asteroids III, ed. F. William, et al., 501–515. Tucson, AZ: University of Arizona Press.
Xiao, Yao, Xiaogang Ruan, and Ruoyan Wei. 2016. Research on the accuracy and operation time of polyhedron gravity model base on 433 Eros. Journal of Deep Space Exploration 3 (1): 41–46.
Jiang, Yu, and Hengnian Li. 2017. Asteroid detector orbital mechanics, 18. Beijing: China Aerospace Publishing House.
Author information
Authors and Affiliations
Corresponding author
Rights and permissions
Copyright information
© 2021 Beijing Institute of Technology Press
About this chapter
Cite this chapter
Wang, D., Li, M., Huang, X., Zhang, X. (2021). Dynamic Models and Environment Models. In: Spacecraft Autonomous Navigation Technologies Based on Multi-source Information Fusion. Space Science and Technologies. Springer, Singapore. https://doi.org/10.1007/978-981-15-4879-6_6
Download citation
DOI: https://doi.org/10.1007/978-981-15-4879-6_6
Published:
Publisher Name: Springer, Singapore
Print ISBN: 978-981-15-4878-9
Online ISBN: 978-981-15-4879-6
eBook Packages: EngineeringEngineering (R0)