David Eagle
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Aerospace engineer (retired) Professional Interests: aerospace trajectory optimization
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Enviada
Lunar Gravity Assist to a Geosynchronous Transfer Orbit
Design an n-body trajectory from low Earth orbit (LEO) to a geosynchronous transfer orbit (GTO) using a gravity assist of the Mo...
11 días hace | 2 descargas |
Enviada
Gravity Perturbed Optimal Orbital Transfer Analysis - SNOPT
Optimal two impulse transfer subject to non-spherical gravity perturbations
alrededor de 2 meses hace | 2 descargas |
Enviada
Gravity Perturbed Optimal Orbital Transfer Analysis - OTB
Optimal two impulse transfer subject to non-spherical gravity perturbations - Optimization Toolbox version
alrededor de 2 meses hace | 3 descargas |
Enviada
Optimal Impulsive Orbital Transfer - SNOPT version
MATLAB script for the solution of the one and two impulse orbit transfer between two Earth orbits.
alrededor de 2 meses hace | 4 descargas |
Enviada
Optimal Impulsive Orbital Transfer - OTB version
MATLAB script for the solution of the one and two impulse orbit transfer between two Earth orbits.
alrededor de 2 meses hace | 11 descargas |
Enviada
Gravity-perturbed Hohmann Transfer - OTB version
MATLAB script that solves the non-spherical gravity-perturbed two impulse Hohmann orbit transfer problem.
2 meses hace | 8 descargas |
Enviada
The Gravity Perturbed Hohmann Transfer - SNOPT version
MATLAB script for solving the Hohmann transfer problem perturbed by non-spherical Earth gravity.
2 meses hace | 7 descargas |
Enviada
MATLAB solutions of Lambert's problem
MATLAB functions and scripts for solving the geocentric and heliocentric Lambert problem.
3 meses hace | 32 descargas |
Enviada
Computer Methods for Aerospace Trajectory Optimization
Additional technical documentation for the Orbital Mechanics with MATLAB scripts posted on the Mathworks File Exchange.
3 meses hace | 4 descargas |
Enviada
MATLAB functions for solving Lambert's problem
Three MATLAB functions and a script that demonstrates how to interact with each Lambert routine.
3 meses hace | 7 descargas |
Enviada
Gravity-Assist with a Powered Flyby - OTB version
MATLAB script that can be used to design and optimize interplanetary trajectories that include a powered flyby gravity assist.
3 meses hace | 3 descargas |
Enviada
Gravity-Assist with a Powered Flyby - SNOPT version
MATLAB script that can be used to design and optimize interplanetary trajectories that include a powered gravity assist.
3 meses hace | 1 descarga |
Enviada
Gravity-assist Trajectory Design and Analysis - SNOPT
A MATLAB Script for Interplanetary Gravity-Assist Trajectory Design and Optimization
4 meses hace | 19 descargas |
Enviada
Parametric Analysis of TLI Delta-V Lunar Transfer
Parametric Analysis of Minimum TLI Delta-V Lunar Transfer Trajectories
5 meses hace | 2 descargas |
Enviada
Parametric Analysis of TLI Delta-V Lunar Trajectories - OTB
Optimization Toolbox version of the tli_sweep MATLAB script that performs a parametric sweep of TLI requirements for Lunar traje...
5 meses hace | 1 descarga |
Enviada
A MATLAB Script for Predicting Equinoxes and Solstices
Predict the calendar date & UTC time of the equinoxes and solstices for a user-defined calendar year
11 meses hace | 2 descargas |
Enviada
Ballistic Interplanetary Trajectory Optimization - OTB
Optimization Toolbox version of the MATLAB script which solves the two impulse, patched-conic interplanetary trajectory problem....
11 meses hace | 9 descargas |
Enviada
Numerical Prediction of Orbital Events
MATLAB script and user's manual for predicting important root-finding and extrema orbital events
alrededor de 1 año hace | 4 descargas |
Enviada
A MATLAB Script for Predicting Solar Eclipses
Predict local circumstances of solar eclipses.
alrededor de 1 año hace | 16 descargas |
Enviada
Propagating Interplanetary Trajectories from Earth to Mars
Numerically integrate the orbital equations of motion of an Earth to Mars interplanetary trajectory.
alrededor de 1 año hace | 8 descargas |
Enviada
A MATLAB Implementation of a Jean Meeus Lunar Algorithm
compute the mean equinox of date position of the moon using the algorithm in chapter 45 of Astronomical Algorithms by Jean Meeus...
alrededor de 1 año hace | 2 descargas |
Enviada
Converting a state vector/orbital elements to a TLE
MATLAB scripts that can be used to calculate an a Two Line Element (TLE) from a user-provided osculating state vector or orbital...
más de 1 año hace | 16 descargas |
Enviada
N-body, Single Gravity-Assist Trajectory Design - SNOPT
Divide-and-conquer approach to solving a single gravity assist interplanetary trajectory subject to n-body perturbations
más de 1 año hace | 2 descargas |
Enviada
N-body, Single Gravity-Assist Trajectory Design - OTB
Divide-and-conquer approach to solving a single gravity assist interplanetary trajectory subject to n-body perturbations
más de 1 año hace | 1 descarga |
Enviada
Geodetic and Geocentric Coordinates
A suite of MATLAB functions for converting between geodetic and geocentric coordinates.
alrededor de 2 años hace | 2 descargas |
Enviada
Halo Orbit Design Using Differential Correction
Script for creating "re-fined" initial conditions for Halo orbits in the Earth-Moon circular-restricted, three-body problem.
alrededor de 2 años hace | 20 descargas |
Enviada
Halo Orbit Design using Richardson's Algorithm
MATLAB script for creating graphic displays of Halo orbits in the circular-restricted, three-body problem.
alrededor de 2 años hace | 27 descargas |
Enviada
Ballistic Trajectory Optimization from Earth to an Asteroid
MATLAB script for optimizing two-body, ballistic trajectories from Earth to the an asteroid.
alrededor de 2 años hace | 6 descargas |
Enviada
The Circular-Restricted Three-Body Problem
Compute and plot characteristics of the circular-restricted three-body problem.
alrededor de 2 años hace | 36 descargas |
Enviada
The Long-term Evolution of Geosynchronous Transfer Orbits
Interactive MATLAB script that predicts the long-term evolution of geosynchronous transfer orbits.
alrededor de 2 años hace | 3 descargas |
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