A Study LEO Satellite Orbit Determination from GPS Data using the Statistical Approach
Article Sidebar
Main Article Content
Abstract
This paper presents a study of the orbit determination of low-Earth orbit (LEO) spacecraft using GPS observable. The statistical approach based on least squares estimation associated with differential correction has been implemented to estimate the position and velocity of the spacecraft. The spacecraft dynamics and orbit perturbation from Earth oblateness, particularly effect, were taken into account. The estimates were evaluated by the conventional orbit propagator.
Article Details
Copyright @2021 Engineering Transactions
Faculty of Engineering and Technology
Mahanakorn University of Technology
References
สมภพ ภูริวิกรัยพงศ์ และสุวัฒน์ กุลธนปรีดา “การคำนวณหาวงโคจรดาวเทียมวงโคจรโลกต่ำ โดยใช้ข้อมูลการวัดสัญญาณจีพีเอส” รายบทความฉบับสมบูรณ์ สนับสนุนโดยสำนักงานคณะกรรมการการอุดมศึกษา และสำนักงานกองทุนสนับสนุนการวิจัย 30 มิถุนายน 2549
E.D. Kaplan and C. Hegarty, Understanding GPS: Principles and Applications, 2nd edition, Artech House, 2005.
R.E. Kalman, “A new approach to linear filtering and prediction problems”, Journal of Basic Engineering, Vol. 82, 1960, pp. 35–45.
F. Gustafsson, and et al., "Particle filters for positioning, navigation, and tracking," Signal Processing, IEEE Transactions on , Vol. 50, No. 2, Feb 2002, pp.425-437.
E.A Wan and R. Van der Merwe, "The unscented Kalman filter for nonlinear estimation", Adaptive Systems for Signal Processing, Communications, and Control Symposium 2000, AS-SPCC The IEEE 2000, pp.153-158.
O. Montenbruck and E. Gill, Satellite Orbits: Models Methods and Applications, Springer, 2011.
D.A. Vallado and W.D. McClain, Fundamentals of Astrodynamics and Applications, 3rd edition, Microcosm Press/Springer, 2007.
D.A. Vollado, and S.S. Carter, Accurate Orbit Determination from Short-arc Dense Observational Data, AS 97-704, AAS/AIAA Astrodynamics Specialist conference, Sun Valley, Idaho, August, 1997.
Y. Hashida, Mathematical Specification of Experimental Orbit Determination of GEO Satellites, Surrey Space Centre, October, 2004.
F.R. Hoots, and R.L. Roehrich, Models for Propagation of NORAD Element Sets, Project Spacetrack Report Number 3, Aerospace Defense Center, December, 1980.
B.W. Parkinson, GPS Performance and Error Analysis, Global Positioning System: Theory and Applications, Vol. 2, 1996, pp. 469-772