Pages that link to "Item:Q1406152"

The following pages link to Analytical treatment of the Earth oblateness and solar radiation pressure effects on an artificial satellite. I: The equations of motion. (Q1406152):

Displaying 12 items.

• Effect of oblateness of an artificial satellite on the orbits around the triangular points of the Earth-Moon system in the axisymmetric ER3BP (Q513381) (← links)
• Modeling of the radial and transverse components of the albedo function (Q1019043) (← links)
• The effect of direct solar radiation pressure on a spacecraft of complex shape. I: The equations of motion. II: The solutions (Q1300514) (← links)
• The joint effect of relativistic and direct solar radiation pressure on an axially symmetric spacecraft. II: The solution and the elements of transformation (Q1406138) (← links)
• The equations of motion of the joint effects of the relativistic and solar radiation pressure on an Earth artificial satellite. (Q1427871) (← links)
• Analytical treatment of the earth oblateness and solar radiation pressure effects on an artificial satellite. II: The solution. (Q1428406) (← links)
• The effects of the terrestrial infrared radiation pressure on the Earth's artificial satellite dynamics (Q1765877) (← links)
• The motion of a geosynchronous satellite. I (Q1819965) (← links)
• The relativistic and direct solar radiation pressure effects on an axially symmetric spacecraft. I: The Hamiltonian and the canonical equations of motion. (Q1855854) (← links)
• Analytical solution to the perturbed \(J_ 2\) motion of artificial satellite in terms of Euler parameters (Q1911221) (← links)
• Phase space description of the dynamics due to the coupled effect of the planetary oblateness and the solar radiation pressure perturbations (Q2005648) (← links)
• Analytical treatment of the relativistic and solar radiation pressure effects on an artificial satellite (Q2493725) (← links)