Title :
Extrapolation and Fitting Algorithms for GLONASS Satellite Orbit
Author :
Hu, Hui ; Yuan, Chao ; Fang, Lian
Author_Institution :
Sch. of Inf. Eng., East China JiaoTong Univ., Nanchang, China
Abstract :
The paper decoded the positioning data, received with GPS & GLONASS receiver of 24 channels (GG24 receiver), to get the orbit parameters of GLONASS satellites at first, and then took these data as initial value for the 4-order Runge-Kutta to orbit extrapolation and compared the extrapolation position with the position in broadcast ephemeris of GLONASS. The experiment indicates that the average positioning error of extrapolation position is less then 1.5 m. Meanwhile, it took Lagrange Interpolation and Chebyshev polynomials fitting these two methods to fitting the satellites´ orbit and compared with the extrapolation, the result indicates that the Chebyshev polynomials fitting could get a small error.
Keywords :
Chebyshev approximation; Global Positioning System; Runge-Kutta methods; curve fitting; extrapolation; satellite navigation; 4-order Runge Kutta method; Chebyshev polynomials; GLONASS satellite orbit; GPS; Lagrange interpolation; average positioning error; broadcast ephemeris; decoded positioning data; extrapolation algorithm; extrapolation position; fitting algorithms; orbit extrapolation; satellites orbit; Acceleration; Chebyshev approximation; Differential equations; Extrapolation; Global Positioning System; Interpolation; Lagrangian functions; Orbital calculations; Polynomials; Satellite broadcasting; 4-order Runge-Kutta; Chebyshev polynomials fitting; Lagrange interpolation; broadcast ephemeris; orbit extrapolation;
Conference_Titel :
Intelligent Information Technology Application, 2009. IITA 2009. Third International Symposium on
Conference_Location :
Nanchang
Print_ISBN :
978-0-7695-3859-4
DOI :
10.1109/IITA.2009.484