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A MATLAB Function for Computing Gravity in the Modified Equinoctial Coordinate System
Computes gravity due to the first four zonal harmonics in the modified equinoctial coordinate system

presque 11 ans il y a | 1 téléchargement |

0.0 / 5

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Solar Sail Trajectory Analysis with MATLAB
Two-dimensional trajectory analysis of solar sail Earth-to-Venus and Earth-to-Mars missions.

presque 11 ans il y a | 1 téléchargement |

4.5 / 5

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MATLAB Functions for Two Body Orbit Propagation
Three MATLAB functions for propagating two-body orbits

environ 11 ans il y a | 1 téléchargement |

5.0 / 5

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Gooding's State Vector-to-Orbital Elements Algorithm
MATLAB demo script and function that implements Gooding's method.

environ 11 ans il y a | 4 téléchargements |

5.0 / 5

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Lunar Free-Return Trajectory Analysis with MATLAB
A MATLAB script for designing two-dimensional lunar free-return trajectories

plus de 11 ans il y a | 1 téléchargement |

0.0 / 5

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

presque 12 ans il y a | 1 téléchargement |

4.0 / 5

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Low Thrust Transfer Between Non-coplanar Circular Orbits
Design and analyze low-thrust orbit transfers

plus de 12 ans il y a | 7 téléchargements |

5.0 / 5

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Repeating Ground Track Orbit Design
Four MATLAB scripts for designing and analyzing repeating ground track orbits.

plus de 12 ans il y a | 1 téléchargement |

5.0 / 5

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Composite Orbit Design
Composite orbits are combinations of orbits that have special geometric & dynamic characteristics.

plus de 12 ans il y a | 2 téléchargements |

5.0 / 5

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Sun-synchronous Orbit Design
Three MATLAB scripts that can be used to design and analyze sun-synchronous Earth orbits.

plus de 12 ans il y a | 2 téléchargements |

5.0 / 5

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Two Impulse Phasing Analysis
Phasing analysis between two coplanar circular orbits using a two impulse Hohmann transfer.

plus de 12 ans il y a | 1 téléchargement |

0.0 / 5

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Circular Orbit Plane Change
MATLAB script for solving the circular orbit plane change problem.

plus de 12 ans il y a | 1 téléchargement |

3.0 / 5

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Mean Local Time of the Ascending Node
Determines the relationship between mean local time of the ascending node and RAAN.

plus de 12 ans il y a | 3 téléchargements |

3.0 / 5

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Low-precision Ephemeris
MATLAB functions that compute a low-precision ephemeris for the Sun, Moon and planets.

plus de 12 ans il y a | 1 téléchargement |

5.0 / 5

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A MATLAB Implementation of the Jacchia Atmosphere Model
MATLAB function and demonstration script which implement the Jacchia 1970 atmosphere model.

plus de 12 ans il y a | 2 téléchargements |

3.0 / 5

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A MATLAB Script for Time and Coordinate Calculations
Interactive MATLAB script that can be used to perform time and coordinate calculations.

plus de 12 ans il y a | 4 téléchargements |

5.0 / 5

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MATLAB Versions of NOVAS
Several NOVAS Fortran subroutines have been ported to MATLAB.

presque 13 ans il y a | 4 téléchargements |

5.0 / 5

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A MATLAB Script for Terrestrial and Celestial Coordinate Conversion
MATLAB functions and script for performing terrestrial to/from celestial coordinate transformations.

environ 13 ans il y a | 2 téléchargements |

0.0 / 5

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A MATLAB Script for Calculating Greenwich Sidereal Time with NOVAS
MATLAB script named demo_sidtim.m and support functions for computing Greenwich sidereal time.

environ 13 ans il y a | 2 téléchargements |

5.0 / 5

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True-of-Date and EME2000 Coordinate Conversion (NOVAS Version)
MATLAB Script for Converting Between True-of-Date and EME2000 Cartesian Coordinates (NOVAS Version)

environ 13 ans il y a | 1 téléchargement |

5.0 / 5

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A MATLAB Implementation of the IAU 2000B Nutation Theory
A MATLAB function and companion script for calculating nutation based on the IAU 2000B theory.

environ 13 ans il y a | 3 téléchargements |

0.0 / 5

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A MATLAB Implementation of the IAU 2000A Nutation Theory
MATLAB function and companion script for computing nutation using the IAU 2000A algorithm.

environ 13 ans il y a | 3 téléchargements |

5.0 / 5

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Cowell's Method for Earth Satellites
MATLAB script for solving the orbital initial value problem (IVP) for satellites in Earth orbit.

environ 13 ans il y a | 7 téléchargements |

5.0 / 5

A soumis

Orbital Periods of a Satellite
MATLAB scripts for computing the orbital periods of a satellite.

environ 13 ans il y a | 2 téléchargements |

0.0 / 5

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A MATLAB Implementation of the IAU 1980 Nutation Theory
MATLAB script and function for computing nutation according to IAU 1980 theory.

environ 13 ans il y a | 7 téléchargements |

0.0 / 5

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A MATLAB Implementation of the JPL Ephemeris
PDF document and MATLAB scripts and functions that evaluate a JPL binary binary ephemeris file.

environ 13 ans il y a | 5 téléchargements |

0.0 / 5

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Orbital Elements of the Moon
MATLAB function that calculates the osculating orbital elements of the Moon.

environ 13 ans il y a | 3 téléchargements |

0.0 / 5

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EME2000 to/from True-of-Date Transformation
This Matlab script converts between true-of-date and EME2000 state vectors using Mice routines.

environ 13 ans il y a | 1 téléchargement |

0.0 / 5

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Precision Sun Ephemeris
Computes true-of-date, geocentric right ascension, declination and position vector of the Sun.

environ 13 ans il y a | 2 téléchargements |

0.0 / 5

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Aeroassist Orbital Transfer
Characteristics of the aeroassist maneuver between two circular, coplanar Earth orbits.

environ 13 ans il y a | 2 téléchargements |

5.0 / 5