Finite-thrust transfer in the two and three body problems Final report
Computer program for optimal finite thrust transfer between two orbits
Engineering topics
Publications and source records attributed to Mc Cue, G. A..
Computer program for optimal finite thrust transfer between two orbits
Computer program for optimization of two-impulse transfers by contouring and steep descent
Quasi-linearization program for boundary value problem of minimum fuel orbital transfer
Quasi-linearization techniques for solving boundary value satellite orbital transfer problems
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Computer method to determine optimum two-impulse orbital transfers between inclined elliptical orbits
Numerical determination of optimum two-impulse orbital transfer between inclined elliptical orbits
Numerical and analytical results on optimum one impulse transfer between coplanar elliptical orbits
Spacecraft rendezvous trajectory between two elliptical orbits is determined by optimization of the two impulse orbital transfer
Optimum two-impulse orbital transfer and rendezvous between any pair of unperturbed elliptical orbits
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