Add to ORKGThe present project will simulate a space launch vehicle trajectory for given launcher and external conditions. It also will give an optimal solution for this trajectory when trajectory parameters are not fixed.Ingeniería Aeroespacia
The conceptual design phase is critical because most of a launch vehicle's life cycle cost is determ...
Introducing the concepts of set-theoretic sequencing logic, hierarchic optimisation and sensitivity-...
This paper compares three different sets of translation equations of motion for a space launcher. Tw...
The present project will simulate a space launch vehicle trajectory for given launcher and external ...
The determination of the trajectory of a space launcher is a complex optimization problem with bound...
Design and simulation of a rocket launcher trajectory, from launch platform to NEO. The present p...
Trajectory optimization of a generic launch vehicle is considered in this paper. The direct applicat...
The optimization of trajectories performed by air-dropped launcher is a new subject in spaceflight o...
In the past few years, a new spirit for the exploration of the Solar System spread among the space c...
ABSTRACT: The use of digital simulation has become an essential activity during the development and ...
This papers introduces an analytic method to define multistage launcher trajectories to determine th...
This work addresses two space trajectory optimization problems: the flight of a launcher upper stage...
Trajectory planning and simulation of docking tests on the ground for space simulator is one of key ...
ABSTRACT: The aim of this study is to model launch vehicles with focus on 3-DOF trajectory optimizat...
The flight control system of a launch vehicle is the result of the right trade-off between different...
The conceptual design phase is critical because most of a launch vehicle's life cycle cost is determ...
Introducing the concepts of set-theoretic sequencing logic, hierarchic optimisation and sensitivity-...
This paper compares three different sets of translation equations of motion for a space launcher. Tw...
The present project will simulate a space launch vehicle trajectory for given launcher and external ...
The determination of the trajectory of a space launcher is a complex optimization problem with bound...
Design and simulation of a rocket launcher trajectory, from launch platform to NEO. The present p...
Trajectory optimization of a generic launch vehicle is considered in this paper. The direct applicat...
The optimization of trajectories performed by air-dropped launcher is a new subject in spaceflight o...
In the past few years, a new spirit for the exploration of the Solar System spread among the space c...
ABSTRACT: The use of digital simulation has become an essential activity during the development and ...
This papers introduces an analytic method to define multistage launcher trajectories to determine th...
This work addresses two space trajectory optimization problems: the flight of a launcher upper stage...
Trajectory planning and simulation of docking tests on the ground for space simulator is one of key ...
ABSTRACT: The aim of this study is to model launch vehicles with focus on 3-DOF trajectory optimizat...
The flight control system of a launch vehicle is the result of the right trade-off between different...
The conceptual design phase is critical because most of a launch vehicle's life cycle cost is determ...
Introducing the concepts of set-theoretic sequencing logic, hierarchic optimisation and sensitivity-...
This paper compares three different sets of translation equations of motion for a space launcher. Tw...