Orbit determination from two position vectors and periapsis radius
Orbit determination from two position vectors and periapsis radius, introducing polar equation for conic to obtain solution
Engineering topics
Publications and source records attributed to Lancaster, E. R..
Orbit determination from two position vectors and periapsis radius, introducing polar equation for conic to obtain solution
Power series solutions of Thiele-Burrau regularized planar restricted three body problem
Unified form of Lambert theorem for elliptic, hyperbolic, and parabolic orbits based on selecting independent variable and normalized time of flight parameter
Approximations to several transcendental functions in universal form of two body problem
Recursion formulas for coefficients of expressions for ratios of geodetic triangles when developed as power series in time intervals
Approximate solution of two-point boundary value problem
Optimized computation with recursive power series integration, applied to three body problem
Power series inverses of universal form of Kepler equation
Recursion formulas for power series inversions of Kepler equation
Iterative interpolation and numerical differentiation using divided differences
Recursion formulas for coefficients of f and g series
Approximations for C and S functions and their derivative functions for application to two-body problem
Coefficients calculated for Taylor series expansion about two points - application of Taylor expansion to two-body problem
Lambert theorem for orbital transfer in elliptic, parabolic and hyperbolic cases
Lambert theorem application to particle motion in gravitational central force field