Add to ORKGPatched conic theory for optimum two-impulse velocity analysis on interplanetary vehicle transfer tr...
The minimum time orbital transfer problem for spacecraft with steerable, continuous thrust of consta...
Quasi-linearization program for boundary value problem of minimum fuel orbital transfe
Optimum transfer between two terminal points for minimum initial impulse under arbitrary initial vel...
Optimum three-impulse transfer from circular Earth parking orbit onto asymptotic velocity vector cha...
Orbit calculation including boundary value problem optimal solution with programming for circular an...
Minimum fuel guidance for time-open rendezvous, orbit transfer, and orbit transfer with tangential n...
Computer program for transfer orbit trajectory optimization based on Lagrange multipliers, Newton-Ra...
This report describes the current state of development of methods for calculating optimal orbital tr...
Predicting characteristics of minimal total impulse solution of two-terminal, two-impulse orbital tr...
For many optimal transfer problems it is reasonable to expect that the minimum time solution is also...
Computational method for two impulse orbital transfer and rendezvous between two elliptical orbit
The Space Exploration Initiative is considering the use of low thrust (nuclear electric, solar elect...
Title from PDF of title page (University of Missouri--Columbia, viewed on July 29, 2013).The entire ...
Two methods of computing coplanar, minimum-fuel, power-limited transfers are developed, based on app...
Patched conic theory for optimum two-impulse velocity analysis on interplanetary vehicle transfer tr...
The minimum time orbital transfer problem for spacecraft with steerable, continuous thrust of consta...
Quasi-linearization program for boundary value problem of minimum fuel orbital transfe
Optimum transfer between two terminal points for minimum initial impulse under arbitrary initial vel...
Optimum three-impulse transfer from circular Earth parking orbit onto asymptotic velocity vector cha...
Orbit calculation including boundary value problem optimal solution with programming for circular an...
Minimum fuel guidance for time-open rendezvous, orbit transfer, and orbit transfer with tangential n...
Computer program for transfer orbit trajectory optimization based on Lagrange multipliers, Newton-Ra...
This report describes the current state of development of methods for calculating optimal orbital tr...
Predicting characteristics of minimal total impulse solution of two-terminal, two-impulse orbital tr...
For many optimal transfer problems it is reasonable to expect that the minimum time solution is also...
Computational method for two impulse orbital transfer and rendezvous between two elliptical orbit
The Space Exploration Initiative is considering the use of low thrust (nuclear electric, solar elect...
Title from PDF of title page (University of Missouri--Columbia, viewed on July 29, 2013).The entire ...
Two methods of computing coplanar, minimum-fuel, power-limited transfers are developed, based on app...
Patched conic theory for optimum two-impulse velocity analysis on interplanetary vehicle transfer tr...
The minimum time orbital transfer problem for spacecraft with steerable, continuous thrust of consta...
Quasi-linearization program for boundary value problem of minimum fuel orbital transfe