Add to ORKGThis report investigates the optimization of time fixed transfer between two elliptical orbits."NASA CR-1508.""February 1970"--Cover.Includes bibliographical references (p. 45-47).This report investigates the optimization of time fixed transfer between two elliptical orbits.Prepared by Stanford University, Stanford, Calif. for National Aeronautics and Space AdministrationMode of access: Internet
International audienceThis paper focuses on the fixed-time minimum-fuel out-of-plane rendezvous betw...
Computational method for time optimal space rendezvous between rocket vehicle and circular orbit tar...
Abstract: In this work the problem of two-impulsive orbital transfers between non-coplanar circular ...
Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. Thesis. 1967. Sc.D.MIC...
Prepared at Langley Research Center."January 1969"--Cover.Includes bibliographical references (p. 56...
International audienceA trajectory optimization problem is examined to determine the most fuel-effic...
This paper aims to analyze optimal rendezvous between two coplanar orbits, seeking to optimize tran...
A method has been developed for determining optimal, i.e. minimum fuel, trajectories for the fixed-t...
The minimum fuel rendezvous problem between several power-limited low-thrust spacecraft neighboring ...
A comparison is made of some methods for calculating ,optimum trajectories. All methods give satis...
Thesis. 1978. Ph.D.--Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics.MI...
Abstract: The four–impulse rendezvous of two spacecrafts moving initially on close near–ci...
"A computer program has been designed which determines the minimum-burn-time, thrusting, transfer tr...
In view of the increasing human activity in space, the maneuvering between different orbits is going...
We are concerned with the general rendezvous problem between two satellites which may be in nonplana...
International audienceThis paper focuses on the fixed-time minimum-fuel out-of-plane rendezvous betw...
Computational method for time optimal space rendezvous between rocket vehicle and circular orbit tar...
Abstract: In this work the problem of two-impulsive orbital transfers between non-coplanar circular ...
Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. Thesis. 1967. Sc.D.MIC...
Prepared at Langley Research Center."January 1969"--Cover.Includes bibliographical references (p. 56...
International audienceA trajectory optimization problem is examined to determine the most fuel-effic...
This paper aims to analyze optimal rendezvous between two coplanar orbits, seeking to optimize tran...
A method has been developed for determining optimal, i.e. minimum fuel, trajectories for the fixed-t...
The minimum fuel rendezvous problem between several power-limited low-thrust spacecraft neighboring ...
A comparison is made of some methods for calculating ,optimum trajectories. All methods give satis...
Thesis. 1978. Ph.D.--Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics.MI...
Abstract: The four–impulse rendezvous of two spacecrafts moving initially on close near–ci...
"A computer program has been designed which determines the minimum-burn-time, thrusting, transfer tr...
In view of the increasing human activity in space, the maneuvering between different orbits is going...
We are concerned with the general rendezvous problem between two satellites which may be in nonplana...
International audienceThis paper focuses on the fixed-time minimum-fuel out-of-plane rendezvous betw...
Computational method for time optimal space rendezvous between rocket vehicle and circular orbit tar...
Abstract: In this work the problem of two-impulsive orbital transfers between non-coplanar circular ...