Abstract:- An orbital maneuver is an important phase of a space mission. The idea is to change the orbit of a spacecraft, in order to be able to complete the mission goals required. It can be done to insert a spacecraft in its nominal orbit or during the mission to compensate undesired effects of perturbations. To perform the orbital maneuvers, a software that calculates an optimal maneuver is developed. This method will be used as a reference for comparison and analises of the suboptimal methods to be used on board. This method id based on an analytical development that generate equations that can be computed in a shorter time, allowing real time applications. In all the simulations, low thrust is used to make the maneuvers
This research is focused on the definition, analysis, and numerical testing an effective orbit contr...
This thesis research has focused on developing an analytical solution for low-thrust transfer orbits...
This handbook provides parametric data useful both to the space vehicle designer and mission analyst...
In this study, low-thrust strategies aimed at the modification of specific orbital elements are inve...
This dissertation presents a method for controlling the orbital elements of a spacecraft using conti...
The study of orbital maneuvers in space missions is a very important problem in astrodynamics. One o...
This paper considers the problem of low thrust suboptimal maneuvers to insert a satellite in a const...
Presented to the 11th Annual Symposium on Graduate Research and Scholarly Projects (GRASP) held at ...
This paper considers the problem of out of plane orbital maneuvers for station keeping of satellites...
This paper investigates two strategies that exploit low-thrust propulsion and natural effects for th...
An approximation of the optimal control law for low-thrust transfers between low-eccentricity orbits...
In this work both reconfiguration and station keeping maneuvers of spacecraft flying in formation wi...
The task of optimizing the space vehicle combined orbital plane change maneuver with the aim of maxi...
In space environment, perturbations make the spacecraft lose its predefined orbit in space. One of t...
In this work both reconfiguration and station keeping maneuvers of spacecraft flying in formation wi...
This research is focused on the definition, analysis, and numerical testing an effective orbit contr...
This thesis research has focused on developing an analytical solution for low-thrust transfer orbits...
This handbook provides parametric data useful both to the space vehicle designer and mission analyst...
In this study, low-thrust strategies aimed at the modification of specific orbital elements are inve...
This dissertation presents a method for controlling the orbital elements of a spacecraft using conti...
The study of orbital maneuvers in space missions is a very important problem in astrodynamics. One o...
This paper considers the problem of low thrust suboptimal maneuvers to insert a satellite in a const...
Presented to the 11th Annual Symposium on Graduate Research and Scholarly Projects (GRASP) held at ...
This paper considers the problem of out of plane orbital maneuvers for station keeping of satellites...
This paper investigates two strategies that exploit low-thrust propulsion and natural effects for th...
An approximation of the optimal control law for low-thrust transfers between low-eccentricity orbits...
In this work both reconfiguration and station keeping maneuvers of spacecraft flying in formation wi...
The task of optimizing the space vehicle combined orbital plane change maneuver with the aim of maxi...
In space environment, perturbations make the spacecraft lose its predefined orbit in space. One of t...
In this work both reconfiguration and station keeping maneuvers of spacecraft flying in formation wi...
This research is focused on the definition, analysis, and numerical testing an effective orbit contr...
This thesis research has focused on developing an analytical solution for low-thrust transfer orbits...
This handbook provides parametric data useful both to the space vehicle designer and mission analyst...