Add to ORKGThe optimization of trajectories performed by air-dropped launcher is a new subject in spaceflight optimization problems. Some analytical formulas are here used to drive numerical algorithms to convergence to optimal solutions. The joint use of analytical formulas (to provide a starting guess) and numerical iterative algorithms provides a flexible tool able to find optimal trajectories for different configurations of launchers dropped with different flight conditions
The paper considers the optimization of earth-based multi-stage rocket interceptors with very short ...
A method for automatically generating approximate trajectories for multistage rockets, launching int...
With the advent of streamlined acquisition processes, such as simulation-based acquisition, the need...
This papers introduces an analytic method to define multistage launcher trajectories to determine th...
The determination of the trajectory of a space launcher is a complex optimization problem with bound...
The present project will simulate a space launch vehicle trajectory for given launcher and external ...
The main goal of this paper is to analyze different methodologies and to quantitatively compare a se...
55 years have passed since the launch of the first man-made space vehicle, Sputnik 1. While spacefli...
In the last decades a number of countries have shown interest towards anti-satellite systems for str...
ABSTRACT: This work describes initial results obtained from an ongoing research involving the develo...
The design of a vehicle launch comprises many factors, including the optimization of the climb path ...
The design of a vehicle launch comprises many factors, including the optimization of the climb path ...
The main goal of any launch vehicle is to bring as much payload to space as possible. Space planes h...
The analytic approach to determine the optimal conditions for maximizing altitude of a sounding rock...
The first part of this study was focused on describe the state-of-art in optimization techniques f...
The paper considers the optimization of earth-based multi-stage rocket interceptors with very short ...
A method for automatically generating approximate trajectories for multistage rockets, launching int...
With the advent of streamlined acquisition processes, such as simulation-based acquisition, the need...
This papers introduces an analytic method to define multistage launcher trajectories to determine th...
The determination of the trajectory of a space launcher is a complex optimization problem with bound...
The present project will simulate a space launch vehicle trajectory for given launcher and external ...
The main goal of this paper is to analyze different methodologies and to quantitatively compare a se...
55 years have passed since the launch of the first man-made space vehicle, Sputnik 1. While spacefli...
In the last decades a number of countries have shown interest towards anti-satellite systems for str...
ABSTRACT: This work describes initial results obtained from an ongoing research involving the develo...
The design of a vehicle launch comprises many factors, including the optimization of the climb path ...
The design of a vehicle launch comprises many factors, including the optimization of the climb path ...
The main goal of any launch vehicle is to bring as much payload to space as possible. Space planes h...
The analytic approach to determine the optimal conditions for maximizing altitude of a sounding rock...
The first part of this study was focused on describe the state-of-art in optimization techniques f...
The paper considers the optimization of earth-based multi-stage rocket interceptors with very short ...
A method for automatically generating approximate trajectories for multistage rockets, launching int...
With the advent of streamlined acquisition processes, such as simulation-based acquisition, the need...