Submitted

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...

ungefär ett år ago | 1 download |

0.0 / 5

Submitted

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...

ungefär ett år ago | 1 download |

0.0 / 5

Submitted

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...

ungefär ett år ago | 1 download |

0.0 / 5

Submitted

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...

ungefär ett år ago | 1 download |

0.0 / 5

Submitted

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...

ungefär ett år ago | 2 downloads |

0.0 / 5

Submitted

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...

ungefär ett år ago | 1 download |

0.0 / 5

Submitted

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

mer än ett år ago | 2 downloads |

0.0 / 5

Submitted

Gravity Perturbed Optimal Orbital Transfer Analysis - OTB
Optimal two impulse transfer subject to non-spherical gravity perturbations - Optimization Toolbox version

mer än ett år ago | 1 download |

0.0 / 5

Submitted

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

mer än ett år ago | 2 downloads |

0.0 / 5

Submitted

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

mer än ett år ago | 9 downloads |

5.0 / 5

Submitted

Gravity-perturbed Hohmann Transfer - OTB version
MATLAB script that solves the non-spherical gravity-perturbed two impulse Hohmann orbit transfer problem.

mer än ett år ago | 1 download |

5.0 / 5

Submitted

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

mer än ett år ago | 1 download |

5.0 / 5

Submitted

MATLAB solutions of Lambert's problem
MATLAB functions and scripts for solving the geocentric and heliocentric Lambert problem.

mer än ett år ago | 12 downloads |

4.7 / 5

Submitted

Computer Methods for Aerospace Trajectory Optimization
Additional technical documentation for the Orbital Mechanics with MATLAB scripts posted on the Mathworks File Exchange.

mer än ett år ago | 2 downloads |

0.0 / 5

Submitted

MATLAB functions for solving Lambert's problem
Three MATLAB functions and a script that demonstrates how to interact with each Lambert routine.

mer än ett år ago | 7 downloads |

0.0 / 5

Submitted

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.

mer än ett år ago | 2 downloads |

0.0 / 5

Submitted

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.

mer än ett år ago | 1 download |

0.0 / 5

Submitted

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

mer än ett år ago | 1 download |

0.0 / 5

Submitted

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

ungefär 2 år ago | 1 download |

0.0 / 5

Submitted

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

mer än 2 år ago | 3 downloads |

5.0 / 5

Submitted

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...

mer än 2 år ago | 1 download |

0.0 / 5

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...

mer än 2 år ago | 14 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

nästan 3 år 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

nästan 3 år ago | 3 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.

mer än 3 år ago | 11 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.

mer än 3 år ago | 6 downloads |

0.0 / 5

Submitted

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

mer än 3 år ago | 5 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.

mer än 3 år ago | 3 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.

mer än 3 år ago | 1 download |

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.

mer än 3 år ago | 7 downloads |

4.7 / 5