Modified multirevolution integration methods for satellite orbit computation

1975 ◽  
Vol 11 (4) ◽  
pp. 433-448 ◽  
Author(s):  
O. F. Graf ◽  
D. G. Bettis
1966 ◽  
Vol 25 ◽  
pp. 363-371
Author(s):  
P. Sconzo

In this paper an orbit computation program for artificial satellites is presented. This program is operational and it has already been used to compute the orbits of several satellites.After an introductory discussion on the subject of artificial satellite orbit computations, the features of this program are thoroughly explained. In order to achieve the representation of the orbital elements over short intervals of time a drag-free perturbation theory coupled with a differential correction procedure is used, while the long range behavior is obtained empirically. The empirical treatment of the non-gravitational effects upon the satellite motion seems to be very satisfactory. Numerical analysis procedures supporting this treatment and experience gained in using our program are also objects of discussion.


1963 ◽  
Vol 51 (2) ◽  
pp. 402-402
Author(s):  
T.R. Benedict

1994 ◽  
Vol 99 (C8) ◽  
pp. 16237 ◽  
Author(s):  
Bruce J. Haines ◽  
George H. Born ◽  
Ronald G. Williamson ◽  
Chester J. Koblinsky

1990 ◽  
Vol 141 ◽  
pp. 155-155
Author(s):  
V.K. Tarady

The attempt was made to determine the corrections to the coefficients of the IAU 1980 nutation series together with other geodesical and geodynamical parameters by the use of the Kiev-Geodynamics-3 program complex for LAGEOS laser data analysis. This complex is based on the MERIT standards and on numerical integration techniques for satellite orbit computation. An integration is carried out in cartesian coordinates by the Adams method of variable step and order.


2015 ◽  
Vol 8 (5) ◽  
pp. 174
Author(s):  
Ayman Hamdy Kassem ◽  
Gamal Mohamad El-Bayoumi ◽  
Tamer Mekky Habib ◽  
Karim Ahmed Kamalaldin

1986 ◽  
Author(s):  
G. HURT ◽  
H. NG ◽  
H. AKIMA ◽  
C. FILIPPI

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