Quasilinearization determination of optimum finite-thrust orbital transfers.
Quasi-linearization determination of optimum finite thrust and impulsive orbital transfers
TRAJECTORY OPTIMIZATION↗
Engineering topics
Mccue, G. A.
Publications and source records attributed to Mccue, G. A..
Optimum thermal design through computer simulation of a space-vehicle structure in earth orbit.
Optimal temperature control design using IBM 7094 digital computer program for thermal environment simulation of stabilized multisurfaced earth- orbiting spacecraft structure
THERMAL SIMULATION↗
Conditions for optimal one-impulse transfer.
Optimal one- and two-impulse orbital transfer maneuvers, considering shallowly intersecting coplanar orbits
OPTIMUM THRUST PROGRAMMING↗
Optimum transfers between nearly tangent orbits.
Impulse functions associated with two-impulse transfer between nearly tangent noncoapsidal coplanar elliptical orbits
ORBITAL TRANSFER↗
Numerical investigation of minimum impulse orbital transfer.
Numerical determination of optimum two-impulse orbital transfers between inclined elliptical orbits
ELLIPTICAL ORBIT↗