[AE - 18] - Orbital Dynamics

0544 Bi-Impulsive Orbital Transfers Between Coplanar Orbits With Minimum Time For A Prescribed Fuel Consumption
0557 Keplerian Elements Evolution in Orbital Maneuvers Through Superposition and Correlated Thrust Vector Deviations
0691 Orbits For Space Debris Considering The Obleteness Of The Earth And The Radiation Pressure
0778 Application Of The Hénon?S Orbit Transfer Problem To Maneuver A Satellite In A Constelation
0808 Eddy Currents Torque Model For Spin Stabilized Earth Spacecraft


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