photo

David Eagle


Last seen: Today Con actividad desde 2012

Followers: 22   Following: 0

Mensaje

Aerospace engineer (retired) Professional Interests: aerospace trajectory optimization

Estadística

File Exchange

156 Archivos

CLASIFICACIÓN
N/A
of 301.726

REPUTACIÓN
N/A

CONTRIBUCIONES
0 Preguntas
0 Respuestas

ACEPTACIÓN DE RESPUESTAS
0.00%

VOTOS RECIBIDOS
0

CLASIFICACIÓN
79 of 21.402

REPUTACIÓN
12.463

EVALUACIÓN MEDIA
4.50

CONTRIBUCIONES
156 Archivos

DESCARGAS
485

ALL TIME DESCARGAS
111500

CLASIFICACIÓN

of 176.285

CONTRIBUCIONES
0 Problemas
0 Soluciones

PUNTUACIÓN
0

NÚMERO DE INSIGNIAS
0

CONTRIBUCIONES
0 Publicaciones

CONTRIBUCIONES
0 Público Canales

EVALUACIÓN MEDIA

CONTRIBUCIONES
0 Temas destacados

MEDIA DE ME GUSTA

  • Explorer
  • Personal Best Downloads Level 4
  • Editor's Pick
  • First Review
  • 5-Star Galaxy Level 5
  • First Submission

Ver insignias

Feeds

Ver por

Enviada


Closest Approach between the Earth and Apophis
MATLAB script for predicting close approach between the Earth and the asteroid Apophis.

alrededor de 6 horas hace | 65 descargas |

0.0 / 5

Enviada


Closest Approach Between the Earth and Heliocentric Objects
MATLAB script that predicts closest approach between the Earth and heliocentric objects.

1 día hace | 1 descarga |

0.0 / 5

Enviada


Graphics Display of Orbital Characteristics of the Planets
Graphics display of the J2000 heliocentric orbital characteristics of the solar system planets.

3 días hace | 2 descargas |

0.0 / 5

Enviada


Graphics Display of the Orbital Characteristics of the Moon
MATLAB script which graphically displays the orbital characteristics of the Moon's geocentric motion.

4 días hace | 3 descargas |

0.0 / 5

Enviada


A MATLAB Script for Computing Hyperbolic Coordinates
This script demonstrates how to compute C3, RLA, and DLA of a hyperbolic orbit.

6 días hace | 2 descargas |

4.0 / 5

Enviada


Earth-to-Mars Interplanetary TCM Optimization - SNOPT
Optimization of interplanetary trajectory correction maneuvers (TCM) during Earth-to-Mars spaceflight using the SNOPT algorithm....

7 días hace | 3 descargas |

0.0 / 5

Enviada


Earth-to-Mars Interplanetary TCM Optimization - OTB
Optimization Toolbox version of the MATLAB script that determines optimal Earth-to-Mars impulsive trajectory correction maneuver...

8 días hace | 2 descargas |

0.0 / 5

Enviada


Trans-Lunar Trajectory Correction Maneuver – SNOPT
Optimize a single impulsive trajectory correction maneuver (TCM) on a trans-lunar trajectory using the SNOPT numerical method.

11 días hace | 2 descargas |

0.0 / 5

Enviada


Trans-Lunar Trajectory Correction Maneuver – OTB
Optimize a single impulsive trajectory correction maneuver (TCM) located on a trans-lunar trajectory.

12 días hace | 3 descargas |

0.0 / 5

Enviada


Trans-Earth Trajectory Correction Maneuver - SNOPT
Optimize a single trans-Earth (Moon-to-Earth) impulsive trajectory correction maneuver (TCM). Target to entry interface (EI) or...

19 días hace | 2 descargas |

0.0 / 5

Enviada


Trans-Earth Trajectory Correction Maneuver – OTB
Optimize a single impulsive trajectory correction maneuver (TCM) on a trans-Earth (Moon-to-Earth) trajectory.

20 días hace | 2 descargas |

0.0 / 5

Enviada


Trans-Lunar Trajectory Optimization – SNOPT
SNOPT version of the tlto script for designing preliminary trans-lunar missions from Earth park orbit to lunar encounter.

23 días hace | 5 descargas |

0.0 / 5

Enviada


Trans-Lunar Trajectory Optimization - OTB
Optimization Toolbox version of the tlto script for designing preliminary trans-lunar missions from Earth park orbit to lunar en...

27 días hace | 8 descargas |

5.0 / 5

Enviada


Parametric Analysis of Trans-Lunar Trajectories (SNOPT)
Parametric Analysis of Minimum TLI Delta-V Lunar Transfer Trajectories

alrededor de 1 mes hace | 3 descargas |

0.0 / 5

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 characteristics for Lunar tr...

alrededor de 1 mes hace | 5 descargas |

0.0 / 5

Enviada


Pork Chop Plots of Ballistic Earth-to-Mars Trajectories
A MATLAB Script for Creating Pork Chop Plots of Ballistic Earth-to-Mars Trajectories

alrededor de 1 mes hace | 23 descargas |

3.0 / 5

Enviada


Ballistic Interplanetary Trajectory Optimization - SNOPT
Design and optimize patched-conic, ballistic interplanetary trajectories between any two planets of our solar system.

alrededor de 2 meses hace | 5 descargas |

0.0 / 5

Enviada


Ballistic Interplanetary Trajectory Optimization - OTB
Optimization Toolbox version of a MATLAB script that solves the two impulse, patched-conic interplanetary trajectory problem.

alrededor de 2 meses hace | 3 descargas |

5.0 / 5

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 | 2 descargas |

0.0 / 5

Enviada


Gravity Perturbed Optimal Orbital Transfer Analysis - SNOPT
Optimal two impulse transfer subject to non-spherical gravity perturbations

alrededor de 2 meses hace | 3 descargas |

0.0 / 5

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 | 2 descargas |

0.0 / 5

Enviada


Optimal Impulsive Orbital Transfer - OTB version
MATLAB script for the solution of the one and two impulse orbital transfer between two Earth orbits.

alrededor de 2 meses hace | 6 descargas |

5.0 / 5

Enviada


Finite-burn raise of a circular or elliptical orbit - SNOPT
This script can be used to model a finite-burn maneuver that raises the perigee or apogee of an initial circular or elliptical o...

3 meses hace | 1 descarga |

0.0 / 5

Enviada


Finite-burn lower of a circular or elliptical orbit - SNOPT
This script can be used to model a finite-burn maneuver that lowers the perigee or apogee of an initial circular or elliptical o...

3 meses hace | 2 descargas |

0.0 / 5

Enviada


Finite-burn circularization of an elliptical orbit - SNOPT
This script circularizes an initial elliptical orbit by performing a finite-burn maneuver at apogee of the initial elliptical or...

3 meses hace | 1 descarga |

0.0 / 5

Enviada


Finite-burn lower of a circular or elliptical orbit - OTB
This script can be used to model a finite-burn maneuver that lowers the perigee or apogee of an initial circular or elliptical o...

3 meses hace | 2 descargas |

0.0 / 5

Enviada


Finite-burn raise of a circular or elliptical orbit - OTB
This script can be used to model a finite-burn maneuver that raises the perigee or apogee of an initial circular or elliptical o...

3 meses hace | 2 descargas |

0.0 / 5

Enviada


Finite-burn circularization of an elliptical orbit - OTB
This script circularizes an initial elliptical orbit by performing a finite-burn maneuver at apogee of the initial elliptical or...

3 meses hace | 2 descargas |

0.0 / 5

Enviada


Numerical Solutions of Kepler's Equation
A demo script for a suite of MATLAB functions for solving Kepler's equation.

4 meses hace | 4 descargas |

4.5 / 5

Enviada


The Gravity Perturbed Hohmann Transfer - SNOPT version
MATLAB script for solving the Hohmann transfer problem perturbed by non-spherical Earth gravity.

4 meses hace | 1 descarga |

5.0 / 5

Cargar más