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

casi 7 años hace | 134 descargas |

0.0 / 5

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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...

más de 7 años hace | 186 descargas |

0.0 / 5

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

más de 10 años hace | 2573 descargas |

0.0 / 5

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

casi 11 años hace | 214 descargas |

0.0 / 5

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

más de 11 años hace | 449 descargas |

0.0 / 5

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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

más de 11 años hace | 319 descargas |

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.

más de 11 años hace | 1274 descargas |

4.5 / 5

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

casi 12 años hace | 2567 descargas |

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.

casi 12 años hace | 878 descargas |

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

más de 12 años hace | 1121 descargas |

0.0 / 5

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

alrededor de 13 años hace | 1942 descargas |

5.0 / 5

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

alrededor de 13 años hace | 1927 descargas |

5.0 / 5

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

alrededor de 13 años hace | 817 descargas |

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.

alrededor de 13 años hace | 1710 descargas |

5.0 / 5

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

más de 13 años hace | 795 descargas |

0.0 / 5

Enviada

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

más de 13 años hace | 791 descargas |

3.0 / 5

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

más de 13 años hace | 1147 descargas |

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.

más de 13 años hace | 1240 descargas |

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.

más de 13 años hace | 2494 descargas |

5.0 / 5

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

casi 14 años hace | 990 descargas |

5.0 / 5

Enviada

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

casi 14 años hace | 1127 descargas |

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.

casi 14 años hace | 1199 descargas |

5.0 / 5

Enviada

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

casi 14 años hace | 1045 descargas |

5.0 / 5

Enviada

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

casi 14 años hace | 584 descargas |

0.0 / 5

Enviada

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

casi 14 años hace | 620 descargas |

5.0 / 5

Enviada

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

casi 14 años hace | 2540 descargas |

5.0 / 5

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

casi 14 años hace | 1024 descargas |

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.

casi 14 años hace | 635 descargas |

0.0 / 5

Enviada

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

casi 14 años hace | 2238 descargas |

0.0 / 5

Enviada

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

casi 14 años hace | 948 descargas |

0.0 / 5