Inviato

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

quasi 11 anni fa | 2 download |

0.0 / 5

Inviato

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

quasi 11 anni fa | 1 download |

0.0 / 5

Inviato

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

quasi 11 anni fa | 3 download |

4.5 / 5

Inviato

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

circa 11 anni fa | 1 download |

5.0 / 5

Inviato

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

circa 11 anni fa | 3 download |

5.0 / 5

Inviato

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

oltre 11 anni fa | 3 download |

0.0 / 5

Inviato

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

circa 12 anni fa | 2 download |

4.0 / 5

Inviato

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

oltre 12 anni fa | 6 download |

5.0 / 5

Inviato

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

oltre 12 anni fa | 2 download |

5.0 / 5

Inviato

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

oltre 12 anni fa | 3 download |

5.0 / 5

Inviato

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

oltre 12 anni fa | 4 download |

5.0 / 5

Inviato

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

oltre 12 anni fa | 1 download |

0.0 / 5

Inviato

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

oltre 12 anni fa | 2 download |

3.0 / 5

Inviato

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

oltre 12 anni fa | 8 download |

3.0 / 5

Inviato

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

oltre 12 anni fa | 4 download |

5.0 / 5

Inviato

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

oltre 12 anni fa | 1 download |

3.0 / 5

Inviato

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

quasi 13 anni fa | 3 download |

5.0 / 5

Inviato

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

circa 13 anni fa | 4 download |

5.0 / 5

Inviato

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

circa 13 anni fa | 2 download |

0.0 / 5

Inviato

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

circa 13 anni fa | 1 download |

5.0 / 5

Inviato

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

circa 13 anni fa | 3 download |

5.0 / 5

Inviato

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

circa 13 anni fa | 4 download |

0.0 / 5

Inviato

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

circa 13 anni fa | 3 download |

5.0 / 5

Inviato

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

circa 13 anni fa | 9 download |

5.0 / 5

Inviato

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

circa 13 anni fa | 2 download |

0.0 / 5

Inviato

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

circa 13 anni fa | 1 download |

0.0 / 5

Inviato

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

circa 13 anni fa | 4 download |

0.0 / 5

Inviato

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

circa 13 anni fa | 1 download |

0.0 / 5

Inviato

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

circa 13 anni fa | 2 download |

0.0 / 5

Inviato

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

circa 13 anni fa | 2 download |

0.0 / 5