Proceedings of the Celestial Mechanics Conference: Outlines of general theories of the Hill-Brown and Delaunay types for orbits of artificial satellites

1958 ◽  
Vol 63 ◽  
pp. 433 ◽  
Author(s):  
D. Brouwer
Keyword(s):  
Celestial Mechanics ◽  
Artificial Satellites ◽  
The Hill

scholarly journals Mathematical Methods Applied to the Celestial Mechanics of Artificial Satellites 2014

2015 ◽  
Vol 2015 ◽  
pp. 1-3
Author(s):  
Antonio F. Bertachini A. Prado ◽  
Josep J. Masdemont ◽  
Maria Cecilia Zanardi ◽  
Silvia Maria Giuliatti Winter ◽  
Tadashi Yokoyama ◽  
...  
Keyword(s):  
Celestial Mechanics ◽  
Artificial Satellites ◽  
Mathematical Methods

scholarly journals Mathematical Methods Applied to the Celestial Mechanics of Artificial Satellites

2012 ◽  
Vol 2012 ◽  
pp. 1-7
Author(s):  
Antonio F. Bertachini A. Prado ◽  
Maria Cecilia Zanardi ◽  
Tadashi Yokoyama ◽  
Silvia Maria Giuliatti Winter ◽  
Josep J. Masdemont
Keyword(s):  
Celestial Mechanics ◽  
Artificial Satellites ◽  
Mathematical Methods

scholarly journals Mathematical Methods Applied to the Celestial Mechanics of Artificial Satellites 2013

2013 ◽  
Vol 2013 ◽  
pp. 1-5 ◽  
Author(s):  
Antonio F. Bertachini A. Prado ◽  
Josep J. Masdemont ◽  
Maria Cecilia Zanardi ◽  
Silvia Maria Giuliatti Winter ◽  
Tadashi Yokoyama ◽  
...  
Keyword(s):  
Celestial Mechanics ◽  
Artificial Satellites ◽  
Mathematical Methods

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.

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