Some qualitative characteristics of near-lunar satellite orbits.
Motion of near lunar satellite in initially circular orbit analyzed by integrating equations for time rates of change of orbit elements
MOTION EQUATION↗
Engineering topics
Tapley, B. D.
Publications and source records attributed to Tapley, B. D..
An optimal terminal guidance method for continuous powered space vehicles.
Error correcting problem in space trajectory of continuous powered space vehicle, discussing optimal terminal guidance
OPTIMAL CONTROL↗