The study presents an analysis of accuracy of observations which are contributing to the maintenance of space object catalogue. After quantifying the uncertainties in optical and radar measurements, the second part of the study presents the error within the mean element orbit determination procedure. A batch least square orbit determination method which makes use of the Draper semi-analytical satellite theory and its partial derivatives is tested for its correctness under catalogue maintenance conditions. Different attributes, which could affect the performance of such an orbit determination method, are identified and examined with real and simulated observations. In conclusion, an analysis of the factors which limit the practical acc...
The Astronomical Institute of the University of Bern (AIUB) is conducting several search campaigns f...
Currently, the number of catalogued space objects in LEO and MEO orbit is about 15000, out of which ...
The precise orbit determination problem is to accurately determine the position and velocity vectors...
The study presents an analysis of the orbit determination process for maintenance of the space objec...
Catalog maintenance for Space Situational Awareness (SSA) demands an accurate and computationally le...
In many cases, we have few optical observations over a short time span, and most of the information ...
Abstract: The main target here is to determine the orbit of an artificial satellite and to analyze i...
The increasing amount of space debris requires huge efforts for the tracking networks in order to...
In calculating the orbit of a minor planet with a least-squares algorithm, current practice is to as...
ABSTRACT Given a set of astrometric observations of the same object, the problem of orbit determinat...
This paper addresses the characterization of the precision of observationally determined orbit param...
Abstract The purpose of this paper was to analyze the modeling of an artificial satellite orbit, usi...
Regular products within the field of Space Surveillance and Tracking (SST) and Space Traffic Managem...
The atmospheric resistance and solar radiation pressure are the main sources of non-gravitational pe...
In calculating the orbit of a minor planet with a least-squares algorithm, current practice is to as...
The Astronomical Institute of the University of Bern (AIUB) is conducting several search campaigns f...
Currently, the number of catalogued space objects in LEO and MEO orbit is about 15000, out of which ...
The precise orbit determination problem is to accurately determine the position and velocity vectors...
The study presents an analysis of the orbit determination process for maintenance of the space objec...
Catalog maintenance for Space Situational Awareness (SSA) demands an accurate and computationally le...
In many cases, we have few optical observations over a short time span, and most of the information ...
Abstract: The main target here is to determine the orbit of an artificial satellite and to analyze i...
The increasing amount of space debris requires huge efforts for the tracking networks in order to...
In calculating the orbit of a minor planet with a least-squares algorithm, current practice is to as...
ABSTRACT Given a set of astrometric observations of the same object, the problem of orbit determinat...
This paper addresses the characterization of the precision of observationally determined orbit param...
Abstract The purpose of this paper was to analyze the modeling of an artificial satellite orbit, usi...
Regular products within the field of Space Surveillance and Tracking (SST) and Space Traffic Managem...
The atmospheric resistance and solar radiation pressure are the main sources of non-gravitational pe...
In calculating the orbit of a minor planet with a least-squares algorithm, current practice is to as...
The Astronomical Institute of the University of Bern (AIUB) is conducting several search campaigns f...
Currently, the number of catalogued space objects in LEO and MEO orbit is about 15000, out of which ...
The precise orbit determination problem is to accurately determine the position and velocity vectors...