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Mean and Osculating Classical Orbital Elements
MATLAB algorithms for converting to/from mean and osculating orbital elements.

2 years 前 | 9 次下载 |

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Low-thrust Earth-to-Mars Trajectory Analysis - SNOPT
Determines optimal, two-dimensional low-thrust Earth-to-Mars interplanetary trajectories.

2 years 前 | 4 次下载 |

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A MATLAB Script for Predicting Orbital Events of the Planets
Predicts interesting orbital events of our solar system planets.

3 years 前 | 2 次下载 |

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A MATLAB script for Earth-to-Mars Mission Design - SNOPT
Design and optimize end-to-end Earth-to-Mars ballistic trajectories from Earth park orbit to Mars B-plane encounter.

3 years 前 | 1 次下载 |

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MATLAB script for Earth-to-Mars Mission Design - OTB
Optimization Toolbox version of the e2m_matlab script that performs Earth-to-Mars mission analysis and design.

3 years 前 | 2 次下载 |

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Graphics Display of the Orbital Characteristics of the Moon
MATLAB script which graphically displays the orbital characteristics of the Moon.

3 years 前 | 1 次下载 |

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Closest Approach Between the Earth and Heliocentric Objects
MATLAB script that predicts closest approach between the Earth and heliocentric objects.

3 years 前 | 1 次下载 |

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Parametric Analysis of Ballistic Earth-to-Mars Trajectories
perform a parametric “sweep” of ballistic interplanetary trajectories from a user-defined Earth park orbit to encounter at Mars

3 years 前 | 1 次下载 |

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A MATLAB Script for Trans-Earth TCM Trajectory Optimization
MATLAB script that can be used to optimize an impulsive trajectory correction maneuver (TCM) during the Trans-Earth phase of lun...

3 years 前 | 1 次下载 |

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Trans-Lunar Trajectory Optimization - OTB/MICE version
Optimization Toolbox version of the tlto_matlab script used to design preliminary lunar missions from Earth park orbit to B-plan...

3 years 前 | 5 次下载 |

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Cowell's Method - MICE Version
PDF document and MATLAB script that demonstrates using Cowell’s method to predict orbital motion.

3 years 前 | 4 次下载 |

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A MATLAB Script for Optimal Single Impulse De-orbit - SNOPT
optimal impulsive maneuver required to de-orbit a spacecraft in a circular or elliptical Earth orbit

4 years 前 | 1 次下载 |

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MATLAB Ephemeris of the Sun and Inner Planets
Analytic ephemeris of the Sun and inner planets (Mercury, Venus and Mars) valid between -4000 B.C. and +2800 A.D.

4 years 前 | 4 次下载 |

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MATLAB Implementation of "Lunar Tables and Programs"
MATLAB demo and function that computes the coordinates of the Moon using algorithms from in "Lunar Tables and Programs".

4 years 前 | 3 次下载 |

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Gravity-perturbed Earth Orbit Lambert Problem - OTB/fsolve
OTB/fsolve version of the lambert4.m MATLAB script which solves the gravity-perturbed Lambert problem

4 years 前 | 1 次下载 |

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Creating a Chebyshev Ephemeris with MATLAB
MATLAB script demonstrates how to create & evaluate a Chebyshev representation of the position coordinates of the sun, a planet ...

4 years 前 | 1 次下载 |

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Solar Sail Trajectory Analysis with MATLAB - OTB version
Optimization Toolbox version for Two-dimensional trajectory analysis of solar sail Earth-to-Venus and Earth-to-Mars missions MAT...

4 years 前 | 1 次下载 |

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Aerospace Trajectory Optimization - OTB
Demonstrates the solution of an aerospace trajectory optimization problem.

4 years 前 | 1 次下载 |

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Graphics Display of Satellite Ground Tracks and Orbits
MATLAB script named satplot.m that demonstrates how to graphically display satellite ground tracks and orbits.

4 years 前 | 6 次下载 |

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Low-thrust Earth to Mars Trajectory Analysis - OTB
Optimization Toolbox version of a MATLAB script that can be used to analyze low-thrust Earth to Mars trajectories.

4 years 前 | 2 次下载 |

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Gravity-perturbed Earth Orbit Lambert Problem - OTB
Optimization Toolbox version of the lambert4.m MATLAB script which solves the gravity-perturbed Lambert problem

4 years 前 | 1 次下载 |

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Lunar Free-Return Trajectory Analysis with MATLAB - OTB
Optimization Toolbox version of the free_return.m MATLAB script which models free-return lunar trajectories.

4 years 前 | 4 次下载 |

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Optimal Single Impulse De-orbit from Earth Orbits - OTB
Optimization Toolbox version of the deorbit.m MATLAB script which determines optimal de-orbit maneuvers.

4 years 前 | 2 次下载 |

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Impulsive Hyperbolic Injection from an Earth Orbit - OTB
Optimization Toolbox version of the hyper2.m MATLAB script which determines the characteristics of hyperbolic injection.

4 years 前 | 1 次下载 |

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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...

5 years 前 | 3 次下载 |

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Computing Phases of the Moon
A MATLAB Script for Computing Phases of the Moon

5 years 前 | 1 次下载 |

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A MATLAB Script for Earth-to-Mars Mission Design
Determines optimal n-body ballistic trajectories from Earth park orbit to encounter at Mars.

6 years 前 | 7 次下载 |

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

8 years 前 | 8 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

8 years 前 | 1 次下载 |

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

9 years 前 | 1 次下载 |