Add to ORKGMassachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. Thesis. 1967. Sc.D.MICROFICHE COPY ALSO AVAILABLE IN AERONAUTICS LIBRARY.Vita.Bibliography: p. 120-122.Sc.D
This paper investigates the use of a genetic algorithm for the optimization of an impulsive multi- ...
The minimum fuel rendezvous problem between several power-limited low-thrust spacecraft neighboring ...
The three-dimensional rendezvous between two spacecraft is considered: a target spacecraft on a circ...
Abstract: The problem of a rendezvous of two spacecrafts on the close near-circular orbits...
A method has been developed for determining optimal, i.e. minimum fuel, trajectories for the fixed-t...
The goal of this paper is to find the number of impulses, value of them and transfer orbit(s) parame...
This report investigates the optimization of time fixed transfer between two elliptical orbits."NASA...
Abstract: The four–impulse rendezvous of two spacecrafts moving initially on close near–ci...
Abstract: The work describes algorithms for minimization in the spaces of impulse componen...
In this article, we focus on safe and effective completion of a rendezvous and docking task by looki...
This work describes the design of an impulsive maneuvers’ planner meant for on-board autonomous opt...
An investigation of a two-impulse plan for performing rendezvous on a once-a-day basis with a near-e...
In this paper, a direct approach is presented to tackle the multi-impulse rendezvous problem conside...
Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1973....
In recent years, there has been a growing demand for the autonomous rendezvous and docking capabilit...
This paper investigates the use of a genetic algorithm for the optimization of an impulsive multi- ...
The minimum fuel rendezvous problem between several power-limited low-thrust spacecraft neighboring ...
The three-dimensional rendezvous between two spacecraft is considered: a target spacecraft on a circ...
Abstract: The problem of a rendezvous of two spacecrafts on the close near-circular orbits...
A method has been developed for determining optimal, i.e. minimum fuel, trajectories for the fixed-t...
The goal of this paper is to find the number of impulses, value of them and transfer orbit(s) parame...
This report investigates the optimization of time fixed transfer between two elliptical orbits."NASA...
Abstract: The four–impulse rendezvous of two spacecrafts moving initially on close near–ci...
Abstract: The work describes algorithms for minimization in the spaces of impulse componen...
In this article, we focus on safe and effective completion of a rendezvous and docking task by looki...
This work describes the design of an impulsive maneuvers’ planner meant for on-board autonomous opt...
An investigation of a two-impulse plan for performing rendezvous on a once-a-day basis with a near-e...
In this paper, a direct approach is presented to tackle the multi-impulse rendezvous problem conside...
Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1973....
In recent years, there has been a growing demand for the autonomous rendezvous and docking capabilit...
This paper investigates the use of a genetic algorithm for the optimization of an impulsive multi- ...
The minimum fuel rendezvous problem between several power-limited low-thrust spacecraft neighboring ...
The three-dimensional rendezvous between two spacecraft is considered: a target spacecraft on a circ...