Add to ORKGIn recent years, there has been a growing demand for the autonomous rendezvous and docking capabilit...
This research describes and applies the recently introduced, general-purpose variable-time-domain ne...
Impulsive solution used to solve optimum trajectory problems with bounded thrust magnitud
For many optimal transfer problems it is reasonable to expect that the minimum time solution is also...
Approximate analytical solution for minimum impulse transfer between circular orbit and given hyperb...
The Space Exploration Initiative is considering the use of low thrust (nuclear electric, solar elect...
AbstractThis article presents a systematic direct approach to carry out effective optimization of a ...
For many problems it is reasonable to expect that the minimum time solution is also the minimum fuel...
Minimum fuel rendezvous guidance of powered interceptor from parking orbit to target in coplanar cir...
The ordinary theory of maxima and minima is applied to develop the optimal switching conditions for ...
The problem considered is that of a three-dimensional, minimum time, heliocentric, Earth-Mars transf...
The word 'rendezvous' implies a pre-arranged meeting between two entities for a specific purpose. Th...
Minimum-fuel trajectories in the Clohessy-Wiltshire orbital model are investigated. Low-thrust varia...
The three-dimensional rendezvous between two spacecraft is considered: a target spacecraft on a circ...
A novel conversion algorithm is presented that combines the fidelity of indirect optimization method...
In recent years, there has been a growing demand for the autonomous rendezvous and docking capabilit...
This research describes and applies the recently introduced, general-purpose variable-time-domain ne...
Impulsive solution used to solve optimum trajectory problems with bounded thrust magnitud
For many optimal transfer problems it is reasonable to expect that the minimum time solution is also...
Approximate analytical solution for minimum impulse transfer between circular orbit and given hyperb...
The Space Exploration Initiative is considering the use of low thrust (nuclear electric, solar elect...
AbstractThis article presents a systematic direct approach to carry out effective optimization of a ...
For many problems it is reasonable to expect that the minimum time solution is also the minimum fuel...
Minimum fuel rendezvous guidance of powered interceptor from parking orbit to target in coplanar cir...
The ordinary theory of maxima and minima is applied to develop the optimal switching conditions for ...
The problem considered is that of a three-dimensional, minimum time, heliocentric, Earth-Mars transf...
The word 'rendezvous' implies a pre-arranged meeting between two entities for a specific purpose. Th...
Minimum-fuel trajectories in the Clohessy-Wiltshire orbital model are investigated. Low-thrust varia...
The three-dimensional rendezvous between two spacecraft is considered: a target spacecraft on a circ...
A novel conversion algorithm is presented that combines the fidelity of indirect optimization method...
In recent years, there has been a growing demand for the autonomous rendezvous and docking capabilit...
This research describes and applies the recently introduced, general-purpose variable-time-domain ne...
Impulsive solution used to solve optimum trajectory problems with bounded thrust magnitud