Application of Brouwer's artificial-satellite theory to computation of the state transition matrix
Application of Brouwer artificial satellite theory to computation of state transition matrix
Engineering topics
Publications and source records attributed to Born, G. H..
Application of Brouwer artificial satellite theory to computation of state transition matrix
Kalman filter set for state vector and observation error variance estimation in discrete- time linear system, using empirical Bayes techniques
Encke type analytical-numerical integration for solving differential equations of modified set of Lagrange planetary equations, obtaining satellite ephemeris for orbit prediction
Short term motion of lunar satellite, discussing third body disturbing functions and perturbation solution of nonsingular orbit elements
Short term motion of lunar satellite, discussing third body disturbing functions and perturbation solution of nonsingular orbit elements
Analytical solutions to spacecraft equations of motion and application to orbit determination
Motion of near lunar satellite in initially circular orbit analyzed by integrating equations for time rates of change of orbit elements
Motion of near lunar satellite in initially circular orbit analyzed by integrating equations for time rates of change of orbit elements
Numerical integration of equations for time rate change of lunar satellite orbits for Apollo project