Prox-1 University-Class Mission to Demonstrate Automated Proximity Operations
Automated Trajectory Control Using Artificial Potential Functions to Target Relative Orbits
Relative Orbital Elements Formulation Based upon the Clohessy-Wiltshire Equations
Relative Orbital Elements Formulation Based upon the Clohessy-Wiltshire Equations
STABILITY OF A DEPLOYABLE DRAG DEVICE FOR SMALL SATELLITE DEORBIT