An analytical state transition matrix and its inverse, which include the short period and secular effects of the second zonal harmonic, were developed from the nonsingular PS satellite theory. The fact that the independent variable in the PS theory is not time is in no respect disadvantageous, since any explicit analytical solution must be expressed in the true or eccentric anomaly. This is shown to be the case for the simple conic matrix. The PS theory allows for a concise, accurate, and algorithmically simple state transition matrix. The improvement over the conic matrix ranges from 2 to 4 digits accuracy
An economical algorithm is presented for predicting the position of a satellite perturbed by drag an...
Differential method of orbit improvement for Vinti spheroidal theory of artificial satellite motion ...
The short and long periodic perturbations and secular perturbation due to the geopotentials of degre...
Application of Brouwer artificial satellite theory to computation of state transition matri
Precision mean element (PME) satellite theories play a key role in orbit dynamics analyses. These th...
This dissertation explores new approaches for modeling perturbed and unperturbed satellite relative ...
<div><p>ABSTRACT In the present study relative state transition matrix was obtained. It matches the ...
Orbital prediction and differential correction using Vintis spheroidal theory for artificial satelli...
The dominant perturbations of the motion of a satellite near the earth are due to atmospheric drag a...
In 1959, Dirk Brouwer pioneered the use of the Hamiltonian perturbation methods for constructing art...
The semi-analytical theory for the motion of a space object replaces the conventional equations of m...
The state transition matrix (STM) is a part of the onboard orbit determination system. It is used to...
International audienceDuring guidance and control procedures of orbiting spacecraft, the respect of ...
Calculation of path deviation of satellite from reference trajectory - perturbation theor
Abstract. This paper investigates the long-period and secular dynamics of a satellite about an oblat...
An economical algorithm is presented for predicting the position of a satellite perturbed by drag an...
Differential method of orbit improvement for Vinti spheroidal theory of artificial satellite motion ...
The short and long periodic perturbations and secular perturbation due to the geopotentials of degre...
Application of Brouwer artificial satellite theory to computation of state transition matri
Precision mean element (PME) satellite theories play a key role in orbit dynamics analyses. These th...
This dissertation explores new approaches for modeling perturbed and unperturbed satellite relative ...
<div><p>ABSTRACT In the present study relative state transition matrix was obtained. It matches the ...
Orbital prediction and differential correction using Vintis spheroidal theory for artificial satelli...
The dominant perturbations of the motion of a satellite near the earth are due to atmospheric drag a...
In 1959, Dirk Brouwer pioneered the use of the Hamiltonian perturbation methods for constructing art...
The semi-analytical theory for the motion of a space object replaces the conventional equations of m...
The state transition matrix (STM) is a part of the onboard orbit determination system. It is used to...
International audienceDuring guidance and control procedures of orbiting spacecraft, the respect of ...
Calculation of path deviation of satellite from reference trajectory - perturbation theor
Abstract. This paper investigates the long-period and secular dynamics of a satellite about an oblat...
An economical algorithm is presented for predicting the position of a satellite perturbed by drag an...
Differential method of orbit improvement for Vinti spheroidal theory of artificial satellite motion ...
The short and long periodic perturbations and secular perturbation due to the geopotentials of degre...