Add to ORKGThe effects of atmosphere drag and zonal harmonics J2 of the gravitational potential of the Cosmos1484 satellite which is near earth orbit has been investigated .Computer simulation at the equation of motion with perturbations using step-by-step integration (Cowell's method ) is designed by matlab a 7.10. position , velocity and range of the satellite
A geostationary transfer orbit (GTO) is typically used to inject spacecraft into the geosta- tionary...
Abstract — This paper is concerned with an orbit prediction using one of the best regular theories (...
The effects of the solar radiation pressure and the attraction of the sun and the moon at high Earth...
Computer simulation of orbit estimation satellites has been developed. The combined effects of the z...
To calculate the position and velocity of the artificial satellite precisely, one has to broil a mat...
The trajectory analysis of a celestial object orbiting another body is the basis for all other, more...
Abstract. Most Keplerian problems were treated as ideal or under the basic assumptions that the moti...
A theory of an Earth satellite has been developed by considering the Earth's bulge, atmospheric drag...
The main point of this paper is to evaluate the perturbations in orbital elements of a low Earth orb...
The report studies some changes in orbital elements of the artificial satellites of Earth under i...
The present investigation deals with the numerical integration of satellite orbits. As the major con...
Although recent numerical studies have demonstrated the possibility to obtain entire families of bou...
Abstract: In this article we present a simple but elegant numerical calculation to study the motion ...
Orbit determination from artificial satellite observations is a key process in obtaining information...
In this paper, we derive the analytical solution of a satellite orbit disturbed by atmospheric drag....
A geostationary transfer orbit (GTO) is typically used to inject spacecraft into the geosta- tionary...
Abstract — This paper is concerned with an orbit prediction using one of the best regular theories (...
The effects of the solar radiation pressure and the attraction of the sun and the moon at high Earth...
Computer simulation of orbit estimation satellites has been developed. The combined effects of the z...
To calculate the position and velocity of the artificial satellite precisely, one has to broil a mat...
The trajectory analysis of a celestial object orbiting another body is the basis for all other, more...
Abstract. Most Keplerian problems were treated as ideal or under the basic assumptions that the moti...
A theory of an Earth satellite has been developed by considering the Earth's bulge, atmospheric drag...
The main point of this paper is to evaluate the perturbations in orbital elements of a low Earth orb...
The report studies some changes in orbital elements of the artificial satellites of Earth under i...
The present investigation deals with the numerical integration of satellite orbits. As the major con...
Although recent numerical studies have demonstrated the possibility to obtain entire families of bou...
Abstract: In this article we present a simple but elegant numerical calculation to study the motion ...
Orbit determination from artificial satellite observations is a key process in obtaining information...
In this paper, we derive the analytical solution of a satellite orbit disturbed by atmospheric drag....
A geostationary transfer orbit (GTO) is typically used to inject spacecraft into the geosta- tionary...
Abstract — This paper is concerned with an orbit prediction using one of the best regular theories (...
The effects of the solar radiation pressure and the attraction of the sun and the moon at high Earth...