The uncertainty in the geopotential model is currently one of the major error sources in the orbit determination of low-altitude Earth-orbiting spacecraft. The results of an investigation of different geopotential error models and modeling approaches currently used for operational orbit error analysis support at the Goddard Space Flight Center (GSFC) are presented, with emphasis placed on sequential orbit error analysis using a Kalman filtering algorithm. Several geopotential models, known as the Goddard Earth Models (GEMs), were developed and used at GSFC for orbit determination. The errors in the geopotential models arise from the truncation errors that result from the omission of higher order terms (omission errors) and the errors in the...
Precision orbit determination methods, along with a new technique to compute relative data weights,...
From simulations, the orbit error can be assumed to be a slowly varying sine wave with a predominant...
Determination of three dimensional orbit accuracy to the 1-cm level is a difficult problem for even ...
An error analysis study was conducted in order to assess the current accuracies and the future antic...
The orbit accuracies needed to support the global crustal dynamics project and recent satellite alti...
Linear estimation theory, along with a new technique to compute relative data weights, was applied t...
Global navigation satellite systems (GNSS) have become the mainstay of transportation systems worldw...
Abstract The purpose of this paper was to analyze the modeling of an artificial satellite orbit, usi...
The earth physics satellite systems error analysis program was applied to the problem of predicting ...
Gravitational field mismodeling procedures errors in the estimated orbital motion of near Earth sate...
Error analysis of distant-satellite-to-close-satellite range-rate, satellite-to-sea altimetry, and g...
For vehicles in orbital cruise, either in orbit around a body or in a transfer orbit, gravity is the...
The computation is described of a geopotential model to deg 360, a sea surface topography model to d...
The applications for which the data from Earth observation satellites can be used are dependent on t...
Precision orbit determination methods, along with a new technique to compute relative data weights,...
Precision orbit determination methods, along with a new technique to compute relative data weights,...
From simulations, the orbit error can be assumed to be a slowly varying sine wave with a predominant...
Determination of three dimensional orbit accuracy to the 1-cm level is a difficult problem for even ...
An error analysis study was conducted in order to assess the current accuracies and the future antic...
The orbit accuracies needed to support the global crustal dynamics project and recent satellite alti...
Linear estimation theory, along with a new technique to compute relative data weights, was applied t...
Global navigation satellite systems (GNSS) have become the mainstay of transportation systems worldw...
Abstract The purpose of this paper was to analyze the modeling of an artificial satellite orbit, usi...
The earth physics satellite systems error analysis program was applied to the problem of predicting ...
Gravitational field mismodeling procedures errors in the estimated orbital motion of near Earth sate...
Error analysis of distant-satellite-to-close-satellite range-rate, satellite-to-sea altimetry, and g...
For vehicles in orbital cruise, either in orbit around a body or in a transfer orbit, gravity is the...
The computation is described of a geopotential model to deg 360, a sea surface topography model to d...
The applications for which the data from Earth observation satellites can be used are dependent on t...
Precision orbit determination methods, along with a new technique to compute relative data weights,...
Precision orbit determination methods, along with a new technique to compute relative data weights,...
From simulations, the orbit error can be assumed to be a slowly varying sine wave with a predominant...
Determination of three dimensional orbit accuracy to the 1-cm level is a difficult problem for even ...