Submitted

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...

3 years ago | 10 downloads |

1.5 / 5

Submitted

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

3 years ago | 1 download |

0.0 / 5

Submitted

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

3 years ago | 2 downloads |

0.0 / 5

Submitted

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.

4 years ago | 13 downloads |

0.0 / 5

Submitted

Halo Orbit Design using Richardson's Algorithm
MATLAB script for creating graphic displays of Halo orbits in the circular-restricted, three-body problem.

4 years ago | 6 downloads |

0.0 / 5

Submitted

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

4 years ago | 11 downloads |

5.0 / 5

Submitted

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

4 years ago | 2 downloads |

5.0 / 5

Submitted

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.

4 years ago | 2 downloads |

0.0 / 5

Submitted

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.

4 years ago | 3 downloads |

4.7 / 5

Submitted

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

4 years ago | 3 downloads |

5.0 / 5

Submitted

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

4 years ago | 10 downloads |

3.0 / 5

Submitted

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

4 years ago | 2 downloads |

0.0 / 5

Submitted

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

4 years ago | 1 download |

0.0 / 5

Submitted

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

4 years ago | 2 downloads |

0.0 / 5

Submitted

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

4 years ago | 4 downloads |

5.0 / 5

Submitted

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

4 years ago | 1 download |

0.0 / 5

Submitted

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...

4 years ago | 1 download |

0.0 / 5

Submitted

Cowell's Method - MICE Version
PDF document and MATLAB script that demonstrates using Cowell’s method to predict orbital motion.

4 years ago | 3 downloads |

0.0 / 5

Submitted

A MATLAB Script for Optimal Single Impulse De-orbit - SNOPT
optimal impulsive maneuver required to de-orbit a spacecraft in a circular or elliptical Earth orbit

6 years ago | 3 downloads |

0.0 / 5

Submitted

MATLAB Ephemeris of the Sun and Inner Planets
Analytic ephemeris of the Sun and inner planets (Mercury, Venus and Mars) valid between -4000 B.C. and +2800 A.D.

6 years ago | 2 downloads |

0.0 / 5

Submitted

Gravity-perturbed Earth Orbit Lambert Problem - OTB/fsolve
OTB/fsolve version of the lambert4.m MATLAB script which solves the gravity-perturbed Lambert problem

6 years ago | 4 downloads |

0.0 / 5

Submitted

Creating a Chebyshev Ephemeris with MATLAB
MATLAB script demonstrates how to create & evaluate a Chebyshev representation of the position coordinates of the sun, a planet ...

6 years ago | 1 download |

0.0 / 5

Submitted

Solar Sail Trajectory Analysis with MATLAB - OTB version
Optimization Toolbox version for Two-dimensional trajectory analysis of solar sail Earth-to-Venus and Earth-to-Mars missions MAT...

6 years ago | 2 downloads |

0.0 / 5

Submitted

Low-thrust Earth to Mars Trajectory Analysis - OTB
Optimization Toolbox version of a MATLAB script that can be used to analyze low-thrust Earth to Mars trajectories.

6 years ago | 1 download |

1.0 / 5

Submitted

Gravity-perturbed Earth Orbit Lambert Problem - OTB
Optimization Toolbox version of the lambert4.m MATLAB script which solves the gravity-perturbed Lambert problem

6 years ago | 2 downloads |

0.0 / 5

Submitted

Optimal Single Impulse De-orbit from Earth Orbits - OTB
Optimization Toolbox version of the deorbit.m MATLAB script which determines optimal de-orbit maneuvers.

6 years ago | 2 downloads |

0.0 / 5

Submitted

A MATLAB Implementation of "Elements of Solar Eclipses"
This is a MATLAB script that implements the numerical methods described in the book "Elements of Solar Eclipses, 1951-2200" by J...

7 years ago | 1 download |

0.0 / 5

Submitted

Low-Thrust Orbital Transfer with Solar-Electric Propulsion
orbital transfer using solar-electric propulsion

10 years ago | 1 download |

0.0 / 5

Submitted

A MATLAB Implementation of the BV78 ODE Solver
Numerical method for solving systems of ODEs using the BV78 algorithm

10 years ago | 1 download |

0.0 / 5

Submitted

Interplanetary Trajectories Using Solar Electric Propulsion
Efficient computation of optimal interplanetary trajectories using solar electric propulsion

11 years ago | 1 download |

0.0 / 5