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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.

11 years 前 | 10 次下载 |

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

11 years 前 | 4 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.

11 years 前 | 2 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.

11 years 前 | 3 次下载 |

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

11 years 前 | 1 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.

11 years 前 | 4 次下载 |

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

11 years 前 | 5 次下载 |

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

11 years 前 | 5 次下载 |

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

11 years 前 | 2 次下载 |

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

11 years 前 | 2 次下载 |

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Single Impulse De-orbit
Two MATLAB scripts that be used to compute the characteristics of single impulse de-orbit maneuvers.

11 years 前 | 1 次下载 |

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A MATLAB Implementation of the SLP96 Ephemeris
MATLAB function and script that demonstrates how to interact with the SLP96 binary ephemeris.

11 years 前 | 1 次下载 |

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Frozen Orbit Design
Two MATLAB scripts for the design and long-term analysis of frozen orbits.

12 years 前 | 4 次下载 |

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Encke's Method
Encke's method for solving the orbital initial value problem (IVP).

12 years 前 | 1 次下载 |

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B-Plane Coordinates
MATLAB script that demonstrates the calculation of b-plane coordinates.

12 years 前 | 1 次下载 |

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Trajectory Modeling in the Flight Path System
Demonstrates how to model the trajectory of aerospace vehicles in the flight path coordinate system.

12 years 前 | 3 次下载 |

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Kepler's Equation
A suite of MATLAB functions for solving Kepler's equation.

12 years 前 | 3 次下载 |

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A MATLAB Script for Designing Interplanetary Launch Trajectories
Preliminary design and analysis of interplanetary launch trajectories.

12 years 前 | 2 次下载 |

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A MATLAB Script for Designing Low-thrust Spiral Trajectories with Constant Periapsis Radius
Design a two-body, low-thrust spiral trajectory with a constant periapsis radius.

12 years 前 | 5 次下载 |