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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

9 years 前 | 1 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.

9 years 前 | 3 次下载 |

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

9 years 前 | 14 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.

9 years 前 | 3 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

10 years 前 | 2 次下载 |

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Impulsive Hyperbolic Injection from a Circular Earth Park Orbit – NLP Method
PDF document and MATLAB script for interplanetary injection using a nonlinear programming method.

10 years 前 | 1 次下载 |

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Aerospace Trajectory Optimization Using Direct Transcription and Collocation
Demonstrates the solution of an aerospace trajectory optimization problem.

10 years 前 | 3 次下载 |

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A MATLAB Script for Predicting Orbital Events of the Moon
A MATLAB script named levents.m that can be used to compute important orbital events of the Moon.

10 years 前 | 1 次下载 |

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

10 years 前 | 2 次下载 |

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Impulsive Hyperbolic Injection from a Circular Earth Park Orbit
Delta-v required for impulsive hyperbolic orbit transfer

10 years 前 | 1 次下载 |

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

11 years 前 | 8 次下载 |

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

11 years 前 | 8 次下载 |

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

11 years 前 | 2 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.

11 years 前 | 7 次下载 |

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

11 years 前 | 2 次下载 |

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

11 years 前 | 3 次下载 |

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

11 years 前 | 3 次下载 |

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

11 years 前 | 11 次下载 |

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

11 years 前 | 6 次下载 |

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

11 years 前 | 2 次下载 |

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

11 years 前 | 3 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.

11 years 前 | 2 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.

11 years 前 | 7 次下载 |

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

11 years 前 | 2 次下载 |

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

11 years 前 | 3 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.

11 years 前 | 3 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.

11 years 前 | 3 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)

11 years 前 | 5 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.

11 years 前 | 1 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.

11 years 前 | 3 次下载 |