Coordinate systems for differential correction
System of state transition partial derivatives for which tracking information normal matrix for lunar orbiter is nearly diagonalized
STATE EQUATION↗
Engineering topics
Publications and source records attributed to Emerson, E. A..
System of state transition partial derivatives for which tracking information normal matrix for lunar orbiter is nearly diagonalized
Error analysis for selecting optimum rates for taking counted doppler rate and range data for tracking short arc of lunar satellite orbit