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.

alrededor de 1 año hace | 3 descargas |

0.0 / 5

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.

alrededor de 1 año hace | 2 descargas |

0.0 / 5

Enviada

Gravity-assist Trajectory Design and Analysis - SNOPT
A MATLAB Script for Interplanetary Gravity-Assist Trajectory Design and Optimization

alrededor de 1 año hace | 13 descargas |

3.7 / 5

Enviada

Parametric Analysis of TLI Delta-V Lunar Transfer
Parametric Analysis of Minimum TLI Delta-V Lunar Transfer Trajectories

más de 1 año hace | 1 descarga |

0.0 / 5

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

casi 2 años hace | 2 descargas |

0.0 / 5

Enviada

Propagating Interplanetary Trajectories from Earth to Mars
Numerically integrate the orbital equations of motion of an Earth to Mars interplanetary trajectory.

alrededor de 2 años hace | 4 descargas |

5.0 / 5

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 2 años hace | 4 descargas |

0.0 / 5

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...

alrededor de 2 años hace | 24 descargas |

1.5 / 5

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 2 años hace | 2 descargas |

0.0 / 5

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 2 años hace | 2 descargas |

0.0 / 5

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 3 años hace | 21 descargas |

0.0 / 5

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 3 años hace | 14 descargas |

0.0 / 5

Enviada

The Circular-Restricted Three-Body Problem
Compute and plot characteristics of the circular-restricted three-body problem.

alrededor de 3 años hace | 10 descargas |

5.0 / 5

Enviada

The Long-term Evolution of Geosynchronous Transfer Orbits
Interactive MATLAB script that predicts the long-term evolution of geosynchronous transfer orbits.

alrededor de 3 años hace | 3 descargas |

5.0 / 5

Enviada

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

alrededor de 3 años 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 TCM maneuvers.

alrededor de 3 años hace | 1 descarga |

0.0 / 5

Enviada

Apparent Position of a Star
PDF document and MATLAB script that computes the geocentric and topocentric apparent position of a star.

alrededor de 3 años hace | 4 descargas |

5.0 / 5

Enviada

Apparent Coordinates of the Moon, Sun or a Planet
MATLAB script that can be used to compute the apparent coordinates of the Moon, Sun or a planet.

alrededor de 3 años hace | 4 descargas |

0.0 / 5

Enviada

A MATLAB Script for Predicting the Evolution of Lunar Orbits
Script for propagating spacecraft lunar orbits subject to non-spherical lunar gravity and third-body gravity.

alrededor de 3 años hace | 5 descargas |

4.7 / 5

Enviada

Propagating Trajectories from the Earth to the Moon
Integrate n-body trajectories from the Earth to the Moon. Includes non-spherical Earth gravity.

alrededor de 3 años hace | 5 descargas |

5.0 / 5

Enviada

Interplanetary, patched-conic gravity assist - OTB version
A MATLAB Script for Interplanetary Patched-Conic, Single Gravity-Assist Trajectory Design, Analysis and Optimization

alrededor de 3 años hace | 5 descargas |

0.0 / 5

Enviada

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

alrededor de 3 años hace | 33 descargas |

3.0 / 5

Enviada

Coverage Characteristics of Earth Satellites
Compute coverage characteristics of single Earth satellites and Walker and user-defined constellations

alrededor de 3 años hace | 7 descargas |

0.0 / 5

Enviada

Predicting Closest Approach of Apophis
MATLAB script for predicting close approaches between the asteroid Apophis and Earth.

alrededor de 3 años hace | 2 descargas |

0.0 / 5

Enviada

Ballistic Interplanetary Trajectory Optimization - SNOPT
A MATLAB Script for Ballistic Interplanetary Trajectory Design and Optimization

alrededor de 3 años hace | 6 descargas |

0.0 / 5

Enviada

Low-thrust Earth-to-Mars Trajectory Analysis - SNOPT
Determines optimal, two-dimensional low-thrust Earth-to-Mars interplanetary trajectories.

alrededor de 3 años hace | 7 descargas |

5.0 / 5

Enviada

A MATLAB script for Earth-to-Mars Mission Design - SNOPT
Design and optimize end-to-end Earth-to-Mars ballistic trajectories from Earth park orbit to Mars B-plane encounter.

más de 3 años hace | 2 descargas |

0.0 / 5

Enviada

MATLAB script for Earth-to-Mars Mission Design - OTB
Optimization Toolbox version of the e2m_matlab script that performs Earth-to-Mars mission analysis and design.

más de 3 años hace | 3 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.

más de 3 años hace | 1 descarga |

0.0 / 5

Enviada

A MATLAB Script for Trans-Earth TCM Trajectory Optimization
MATLAB script that can be used to optimize an impulsive trajectory correction maneuver (TCM) during the Trans-Earth phase of lun...

más de 3 años hace | 1 descarga |

0.0 / 5