Add to ORKGA comparison is made of some methods for calculating ,optimum trajectories. All methods give satisfactory results but the results are generally favorable to a differential method based on Bliss's differential techniques
This research describes and applies the recently introduced, general-purpose variable-time-domain ne...
It is well known that the use of aerodynamic forces to assist in orbital transfer can significantly ...
This report investigates the optimization of time fixed transfer between two elliptical orbits."NASA...
Abstract: In this work, two direct methods of low-thrust trajectory optimization are imple...
The aim of this thesis is to provide a number of tools and methodologies that allow the designer to ...
In this chapter, a general methodology to apply the theory of optimal control to spacecraft trajecto...
In this paper we present, a comparison of trajectory optimization approaches for the minimum fuel re...
The three-dimensional rendezvous between two spacecraft is considered: a target spacecraft on a circ...
Abstract: The work describes algorithms for minimization in the spaces of impulse componen...
International audienceA trajectory optimization problem is examined to determine the most fuel-effic...
This thesis discusses optimal trajectories for hypervelocity flight of interest in aeroassisted orbi...
A method for determining the optimal impulsive trajectories is applied to minimum fuel, direct ascen...
The work presented in this thesis is concerned with certain problems in the domain of optimal trajec...
Abstract: The four–impulse rendezvous of two spacecrafts moving initially on close near–ci...
The word 'rendezvous' implies a pre-arranged meeting between two entities for a specific purpose. Th...
This research describes and applies the recently introduced, general-purpose variable-time-domain ne...
It is well known that the use of aerodynamic forces to assist in orbital transfer can significantly ...
This report investigates the optimization of time fixed transfer between two elliptical orbits."NASA...
Abstract: In this work, two direct methods of low-thrust trajectory optimization are imple...
The aim of this thesis is to provide a number of tools and methodologies that allow the designer to ...
In this chapter, a general methodology to apply the theory of optimal control to spacecraft trajecto...
In this paper we present, a comparison of trajectory optimization approaches for the minimum fuel re...
The three-dimensional rendezvous between two spacecraft is considered: a target spacecraft on a circ...
Abstract: The work describes algorithms for minimization in the spaces of impulse componen...
International audienceA trajectory optimization problem is examined to determine the most fuel-effic...
This thesis discusses optimal trajectories for hypervelocity flight of interest in aeroassisted orbi...
A method for determining the optimal impulsive trajectories is applied to minimum fuel, direct ascen...
The work presented in this thesis is concerned with certain problems in the domain of optimal trajec...
Abstract: The four–impulse rendezvous of two spacecrafts moving initially on close near–ci...
The word 'rendezvous' implies a pre-arranged meeting between two entities for a specific purpose. Th...
This research describes and applies the recently introduced, general-purpose variable-time-domain ne...
It is well known that the use of aerodynamic forces to assist in orbital transfer can significantly ...
This report investigates the optimization of time fixed transfer between two elliptical orbits."NASA...