Add to ORKGMathematical model for near-body orbit calculation using mass concentration, perturbation theory, nonlinear equations, geopotentials, and least squares metho
Methods of orbital position estimation were reviewed. The problem of accuracy in orbital mechanics i...
Celestial mechanics perturbation methods applied to problem of describing motion of rigid artificial...
Precise relative position determination of satellite formation elements in near circular orbits is t...
The observations of a near-body satellite are used in the determination of certain constants appeari...
Orbit calculation including boundary value problem optimal solution with programming for circular an...
A multivariate optimisation technique for refining the physical characteristics and non-natural beha...
The problem of the two-body gravitational interaction has been solved numerically based on the class...
Precision mean element (PME) satellite theories play a key role in orbit dynamics analyses. These th...
Abstract: The motion of an artificial Earth satellite is continually under varying perturbations cau...
The conference emphasizes orbital position estimation and trajectory calculation methods that consid...
Spacecraft flying in close proximity of small bodies face a very complex dynamical environment with ...
Mathematical and algorithmical techniques for solution of problems in satellite dynamics were develo...
The stability of the nonlinear dynamical system of two GRAVSAT - type satellites was investigated by...
Comparison of theoretical and measured orbital perturbations of artificial earth satellite
While the use of relative orbit determination has reduced the difficulties inherent in tracking geos...
Methods of orbital position estimation were reviewed. The problem of accuracy in orbital mechanics i...
Celestial mechanics perturbation methods applied to problem of describing motion of rigid artificial...
Precise relative position determination of satellite formation elements in near circular orbits is t...
The observations of a near-body satellite are used in the determination of certain constants appeari...
Orbit calculation including boundary value problem optimal solution with programming for circular an...
A multivariate optimisation technique for refining the physical characteristics and non-natural beha...
The problem of the two-body gravitational interaction has been solved numerically based on the class...
Precision mean element (PME) satellite theories play a key role in orbit dynamics analyses. These th...
Abstract: The motion of an artificial Earth satellite is continually under varying perturbations cau...
The conference emphasizes orbital position estimation and trajectory calculation methods that consid...
Spacecraft flying in close proximity of small bodies face a very complex dynamical environment with ...
Mathematical and algorithmical techniques for solution of problems in satellite dynamics were develo...
The stability of the nonlinear dynamical system of two GRAVSAT - type satellites was investigated by...
Comparison of theoretical and measured orbital perturbations of artificial earth satellite
While the use of relative orbit determination has reduced the difficulties inherent in tracking geos...
Methods of orbital position estimation were reviewed. The problem of accuracy in orbital mechanics i...
Celestial mechanics perturbation methods applied to problem of describing motion of rigid artificial...
Precise relative position determination of satellite formation elements in near circular orbits is t...