Submitted


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

mer än 10 år ago | 12 downloads |

Submitted


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

mer än 10 år ago | 8 downloads |

Submitted


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

mer än 10 år ago | 3 downloads |

Submitted


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

mer än 10 år ago | 19 downloads |

Submitted


Modeling Aero-assist Flight Mechanics with MATLAB
Numerically integrate the flight path equations of motion of an aero-assist vehicle.

mer än 10 år ago | 5 downloads |

Submitted


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

mer än 10 år ago | 1 download |

Submitted


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

mer än 10 år ago | 4 downloads |

Submitted


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

mer än 10 år ago | 16 downloads |

Submitted


The Hohmann Orbit Transfer
Computes characteristics for coplanar and non-coplanar Hohmann transfers.

mer än 10 år ago | 23 downloads |

Submitted


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

mer än 10 år ago | 1 download |

Submitted


Bi-elliptic Transfer Between Coplanar Circular Orbits
Bi-elliptic orbital transfer between two coplanar circular Earth orbits.

mer än 10 år ago | 3 downloads |

Submitted


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

nästan 11 år ago | 5 downloads |

Submitted


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

nästan 11 år ago | 7 downloads |

Submitted


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

ungefär 11 år ago | 2 downloads |

Submitted


Selenocentric Coordinates and Transformations
MATLAB functions for computing selenocentric (moon-centered) coordinates and transformations.

ungefär 11 år ago | 2 downloads |

Submitted


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

ungefär 11 år ago | 7 downloads |

Submitted


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

ungefär 11 år ago | 3 downloads |

Submitted


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

ungefär 11 år ago | 3 downloads |

Submitted


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

ungefär 11 år ago | 1 download |

Submitted


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

ungefär 11 år ago | 3 downloads |

Submitted


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

ungefär 11 år ago | 6 downloads |

Submitted


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

ungefär 11 år ago | 1 download |

Submitted


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

mer än 11 år ago | 1 download |

Submitted


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

mer än 11 år ago | 6 downloads |

Submitted


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

mer än 11 år ago | 3 downloads |

Submitted


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

mer än 11 år ago | 3 downloads |

Submitted


Ephemeris Calculations with MICE
Demonstrates ephemeris calculations using the MATLAB version of the JPL Spice library (MICE).

mer än 11 år ago | 11 downloads |

Submitted


Selenocentric Coordinates and Transformations
MATLAB scripts and functions for computing useful selenocentric coordinates and transformations.

mer än 11 år ago | 2 downloads |

Submitted


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

mer än 11 år ago | 1 download |

Submitted


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

mer än 11 år ago | 2 downloads |

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