Optimum trajectory with specified transfer angle between two terminals in an inverse square gravitational field is investigated, criterion of optimization being minimum velocity increment at the initial terminal. Results are numerically illustrated for two orbits in Earth's gravitational field
The problem of many revolution low-thrust Earth-orbit trajectory optimization is considered. The obj...
Within the field of trajectory optimisation, Lawden developed the primer vector theory, which define...
This thesis considers both classical and minimax problems of optimal control arising in the study of...
Optimum trajectory with specified transfer angle between two terminals in an inverse square gravita...
Inter-orbital optimum trajectories with specified transfer angle in an inverse square gravitational ...
Transfer Trajectories between circular orbits in an inverse square gravitational field are investiga...
Minimal exit trajectories with optimum correctional manoeuvers to a rocket between two coplaner, non...
Rocket trajectories in a gravitational field between two terminals with specified velocities at each...
Abstract: Low-thrust maneuvers from high-elliptical orbits are of peculiar interest becaus...
This thesis discusses optimal trajectories for hypervelocity flight of interest in aeroassisted orbi...
The problem of many revolution low-thrust Earth-orbit trajectory optimization is considered. The obj...
Within the field of trajectory optimisation, Lawden developed the primer vector theory, which define...
This thesis considers both classical and minimax problems of optimal control arising in the study of...
Optimum trajectory with specified transfer angle between two terminals in an inverse square gravita...
Inter-orbital optimum trajectories with specified transfer angle in an inverse square gravitational ...
Transfer Trajectories between circular orbits in an inverse square gravitational field are investiga...
Minimal exit trajectories with optimum correctional manoeuvers to a rocket between two coplaner, non...
Rocket trajectories in a gravitational field between two terminals with specified velocities at each...
Abstract: Low-thrust maneuvers from high-elliptical orbits are of peculiar interest becaus...
This thesis discusses optimal trajectories for hypervelocity flight of interest in aeroassisted orbi...
The problem of many revolution low-thrust Earth-orbit trajectory optimization is considered. The obj...
Within the field of trajectory optimisation, Lawden developed the primer vector theory, which define...
This thesis considers both classical and minimax problems of optimal control arising in the study of...
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