Add to ORKGKinematic orbits provide a time series of independent positions, which are a good base for gravity field recovery. Gravity field recovery using the energy integral requires numerical differentiation in order to get velocity information for kinetic energy. This paper deals with numerical differentiation methods to test the most effective method for velocity determination of a LEO (Low Earth Orbiter)
Gravity field determination using the measurements of Global Positioning receivers onboard low Earth...
Gravity field reconstruction via the analysis of kinematic orbit positions has been proven to provi...
International audienceVarious methods for kinematic and reduced-dynamic precise orbit determination ...
Kinematic orbits provide a time series of independent positions, which are a good base for gravity f...
textThe historical method of precise orbit determination is a dynamic approach. However, with the im...
Classical numerical integration methods have been tested for determining the orbit of most recent Lo...
The so-called highly reduced-dynamic (HRD) orbit determination strategy and its use for the determin...
Some interpolation and smoothing techniques have been analyzed for velocity and acceleration determi...
The geometrical point-wise satellite positions can be derived by GNSS analysis techniques. The diffe...
The geometrical point-wise satellite positions can be derived by GNSS analysis techniques. The diffe...
The interest in a precise orbit determination of Low Earth Orbiters (LEOs) using GNSS observations t...
A fast iterative method for gravity field determination from low Earth satellite orbit coordinates h...
International audienceAn algorithm for the (kinematic) orbit analysis of a Low Earth Orbiting (LEO) ...
SST (Satellite to Satellite Tracking) observations between GPS and LEO (Low Earth Orbiter) play an i...
Very precise kinematic or dynamic orbits based on measurements of the Global Navigation Satellite Sy...
Gravity field determination using the measurements of Global Positioning receivers onboard low Earth...
Gravity field reconstruction via the analysis of kinematic orbit positions has been proven to provi...
International audienceVarious methods for kinematic and reduced-dynamic precise orbit determination ...
Kinematic orbits provide a time series of independent positions, which are a good base for gravity f...
textThe historical method of precise orbit determination is a dynamic approach. However, with the im...
Classical numerical integration methods have been tested for determining the orbit of most recent Lo...
The so-called highly reduced-dynamic (HRD) orbit determination strategy and its use for the determin...
Some interpolation and smoothing techniques have been analyzed for velocity and acceleration determi...
The geometrical point-wise satellite positions can be derived by GNSS analysis techniques. The diffe...
The geometrical point-wise satellite positions can be derived by GNSS analysis techniques. The diffe...
The interest in a precise orbit determination of Low Earth Orbiters (LEOs) using GNSS observations t...
A fast iterative method for gravity field determination from low Earth satellite orbit coordinates h...
International audienceAn algorithm for the (kinematic) orbit analysis of a Low Earth Orbiting (LEO) ...
SST (Satellite to Satellite Tracking) observations between GPS and LEO (Low Earth Orbiter) play an i...
Very precise kinematic or dynamic orbits based on measurements of the Global Navigation Satellite Sy...
Gravity field determination using the measurements of Global Positioning receivers onboard low Earth...
Gravity field reconstruction via the analysis of kinematic orbit positions has been proven to provi...
International audienceVarious methods for kinematic and reduced-dynamic precise orbit determination ...