Pages that link to "Item:Q1038757"

The following pages link to Attitude stability of artificial satellites subject to gravity gradient torque (Q1038757):

Displaying 9 items.

• Corrections stemming from the non-osculating character of the Andoyer variables used in the description of rotation of the elastic Earth (Q362664) (← links)
• Modeling and numerical simulation of linear and nonlinear spacecraft attitude dynamics and gravity gradient moments: a comparative study (Q430373) (← links)
• Stabilization of the solar orientation mode of an artificial satellite of the Earth without accumulation of the angular momentum of the gyro system (Q786176) (← links)
• Investigation of equilibria of a satellite subjected to gravitational and aerodynamic torques (Q871314) (← links)
• Long time stability for the main problem of artificial satellites (Q1286897) (← links)
• Electrodynamic stabilization of artificial Earth satellites in the König coordinate system (Q1743046) (← links)
• Gravitational stabilization of a satellite using a movable mass (Q2331270) (← links)
• The triaxiality role in the spin-orbit dynamics of a rigid body (Q2690583) (← links)
• A first order automated Lie transform (Q2800665) (← links)