Engineering topics
Breakwell, J. V.
Publications and source records attributed to Breakwell, J. V..
Rigorous error bounds on position and velocity in satellite orbit theories
Rigorous error bounds on position and velocity for satellite orbits with eccentricity of less than one
An investigation of high eccentricity orbits about Mars
Possible long-period fluctuations, due to solar gravitational field, in radius of pericenter of orbiter of Mars
Rigorous error bounds on position and velocity in satellite orbit theories.
Rigorous error bounds on position and velocity of satellite derived from Hamiltonian theory and von Zeipel method
Satellite orbit studies
Earth-satellite orbits in resonance with tesseral perturbation, and motion near earth-moon libration point
Rigorous error bounds on position and velocity in satellite orbit theories.
Rigorous error bounds on position and velocity of satellite derived from Hamiltonian theory and von Zeipel method
Rigorous Error Bounds on Position and Velocity in Satellite Orbit Theories
Error bounds on position and velocity in satellite orbit theories
Optimum guidance for a low thrust interplanetary vehicle.
Optimum guidance in two dimensions of constant acceleration low-thrust vehicle spiraling away from and in toward planet
Theory of minimum effort control
Optimum control theory formulations for solving problems in optimum guidance for interplanetary manned space flight missions
Nonlinear resonance affecting gravity-gradient stability.
Nonlinear resonance effect on attitude librations of undamped rigid gravity gradient stabilized satellite in circular Earth orbit
Application of the continuous and discrete strategies of minimum effort theory to interplanetary guidance.
Minimum effort theory for interplanetary spacecraft guidance and control
Optimum guidance for a low thrust interplanetary vehicle.
Optimum guidance in two dimensions of constant acceleration low-thrust vehicle spiraling away from and in toward planet
TRAJECTORIES LAUNCHED NORMAL TO THE ECLIPTIC
One-dimensional approximate analysis of the motion of a vehicle launched normal to the ecliptic at relatively low escape speed