Add to ORKGOptimum transfer between two terminal points for minimum initial impulse under arbitrary initial velocity vecto
Inter-orbital optimum trajectories with specified transfer angle in an inverse square gravitational ...
In view of the increasing human activity in space, the maneuvering between different orbits is going...
The problem of minimization of fuel consumption during the atmospheric portion of an aeroassisted, o...
Patched conic theory for optimum two-impulse velocity analysis on interplanetary vehicle transfer tr...
http://deepblue.lib.umich.edu/bitstream/2027.42/7824/5/bad2634.0001.001.pdfhttp://deepblue.lib.umich...
Predicting characteristics of minimal total impulse solution of two-terminal, two-impulse orbital tr...
"November, 1966."Includes bibliographical references."Prepared under grant no.Mode of access: Intern...
Approximate analytical solution for minimum impulse transfer between circular orbit and given hyperb...
Optimum three-impulse transfer from circular Earth parking orbit onto asymptotic velocity vector cha...
A method developed to compute two-body, optimal, N-impulse trajectories was presented. The necessary...
The first part of the paper presents some closed-form solutions to the optimal two-impulse transfer ...
This thesis discusses optimal trajectories for hypervelocity flight of interest in aeroassisted orbi...
This paper introduces a mathematical model that can be used to evaluate the total velocity variation...
Within the field of trajectory optimisation, Lawden developed the primer vector theory, which define...
The aim of this paper is to propose a semi-analytical method for the analysis of a two-impulse trans...
Inter-orbital optimum trajectories with specified transfer angle in an inverse square gravitational ...
In view of the increasing human activity in space, the maneuvering between different orbits is going...
The problem of minimization of fuel consumption during the atmospheric portion of an aeroassisted, o...
Patched conic theory for optimum two-impulse velocity analysis on interplanetary vehicle transfer tr...
http://deepblue.lib.umich.edu/bitstream/2027.42/7824/5/bad2634.0001.001.pdfhttp://deepblue.lib.umich...
Predicting characteristics of minimal total impulse solution of two-terminal, two-impulse orbital tr...
"November, 1966."Includes bibliographical references."Prepared under grant no.Mode of access: Intern...
Approximate analytical solution for minimum impulse transfer between circular orbit and given hyperb...
Optimum three-impulse transfer from circular Earth parking orbit onto asymptotic velocity vector cha...
A method developed to compute two-body, optimal, N-impulse trajectories was presented. The necessary...
The first part of the paper presents some closed-form solutions to the optimal two-impulse transfer ...
This thesis discusses optimal trajectories for hypervelocity flight of interest in aeroassisted orbi...
This paper introduces a mathematical model that can be used to evaluate the total velocity variation...
Within the field of trajectory optimisation, Lawden developed the primer vector theory, which define...
The aim of this paper is to propose a semi-analytical method for the analysis of a two-impulse trans...
Inter-orbital optimum trajectories with specified transfer angle in an inverse square gravitational ...
In view of the increasing human activity in space, the maneuvering between different orbits is going...
The problem of minimization of fuel consumption during the atmospheric portion of an aeroassisted, o...