Modified multirevolution integration methods for satellite orbit computation

1975 ◽  
Vol 11 (4) ◽  
pp. 433-448 ◽  
Author(s):  
O. F. Graf ◽  
D. G. Bettis
Keyword(s):  
Satellite Orbit ◽  
Integration Methods ◽  
Orbit Computation

Artificial satellite orbit computations

1966 ◽  
Vol 25 ◽  
pp. 363-371
Author(s):  
P. Sconzo
Keyword(s):  
Artificial Satellite ◽  
Satellite Orbit ◽  
Artificial Satellites ◽  
Orbital Elements ◽  
Differential Correction ◽  
Gravitational Effects ◽  
Short Intervals ◽  
The Subject ◽  
Introductory Discussion ◽  
Orbit Computation

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.

Rapid satellite orbit computation

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

Application of the GEM-T2 gravity field to altimetric satellite orbit computation

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

scholarly journals Corrections to the IAU 1980 Nutation Series From Lageos Observations

1990 ◽  
Vol 141 ◽  
pp. 155-155
Author(s):  
V.K. Tarady
Keyword(s):  
Data Analysis ◽  
Numerical Integration ◽  
Satellite Orbit ◽  
Program Complex ◽  
Adams Method ◽  
Laser Data ◽  
Variable Step ◽  
Integration Techniques ◽  
Nutation Series ◽  
Orbit Computation

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.

Improving Satellite Orbit Estimation Using Commercial Cameras

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

Geostationary Satellite Orbit Analysis Program (OSOAP)

1986 ◽  
Author(s):  
G. HURT ◽  
H. NG ◽  
H. AKIMA ◽  
C. FILIPPI
Keyword(s):  
Satellite Orbit ◽  
Geostationary Satellite ◽  
Analysis Program ◽  
Orbit Analysis
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