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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...

7 years 前 | 168 次下载 |

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

10 years 前 | 2570 次下载 |

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

10 years 前 | 214 次下载 |

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

11 years 前 | 449 次下载 |

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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

11 years 前 | 318 次下载 |

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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.

11 years 前 | 1271 次下载 |

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

12 years 前 | 2564 次下载 |

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

12 years 前 | 878 次下载 |

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

12 years 前 | 1119 次下载 |

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

13 years 前 | 1939 次下载 |

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

13 years 前 | 1924 次下载 |

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

13 years 前 | 816 次下载 |

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

13 years 前 | 1710 次下载 |

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

13 years 前 | 793 次下载 |

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

13 years 前 | 790 次下载 |

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

13 years 前 | 1146 次下载 |

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

13 years 前 | 1236 次下载 |

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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.

13 years 前 | 2471 次下载 |

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

13 years 前 | 973 次下载 |

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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.

13 years 前 | 1126 次下载 |

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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.

13 years 前 | 1181 次下载 |

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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)

13 years 前 | 1043 次下载 |

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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.

13 years 前 | 583 次下载 |

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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.

13 years 前 | 619 次下载 |

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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.

13 years 前 | 2538 次下载 |

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

13 years 前 | 1024 次下载 |

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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.

13 years 前 | 632 次下载 |

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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.

13 years 前 | 2234 次下载 |

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

14 years 前 | 947 次下载 |

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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.

14 years 前 | 737 次下载 |

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