Optimum guidance for a low thrust interplanetary vehicle.
A direct and analytical solution for space flight guidance functions.
The flight path control software system of the Lunar Orbiter.
Optimization problems caused by interaction of guidance and propellant systems.
Optimization problems caused by interaction of guidance and propellant systems.
A general method for determining optimum thrust nozzle contours for gas-particle flows.
Optimal and suboptimal guidance and control for low thrust orbital transfer.
A statistical optimization of the two-impulse transfer maneuver for a fixed-time rendezvous.
Rapid determination of near-optimum linear pitch programs for rocket boosters.
Optimization of data return from planetary missions by trajectory design.
A manual optimal guidance scheme using a predictive model.
Optimal payload trajectory characteristics for winged booster vehicles.
Automatic design of optimum Atlas-Agena vehicle trajectories.
Research relating to long-range supersonic cruising aircraft.