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Predicting Local Circumstances of Lunar Eclipses
Predict the local circumstances (times and topocentric coordinates of the Moon) of lunar eclipses.

etwa ein Jahr vor | 2 Downloads |

0.0 / 5

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Predicting Local Circumstances of Lunar Occultations
Predict the local circumstances (topocentric azimuth and elevation) of lunar occultations of a planet or star.

etwa ein Jahr vor | 1 Download |

0.0 / 5

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Flight Performance of a Single Stage Rocket
Predict the maximum altitude and "best" liftoff mass of a single stage rocket.

etwa ein Jahr vor | 4 Downloads |

0.0 / 5

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

etwa ein Jahr vor | 1 Download |

0.0 / 5

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Graphics Display of Orbital Characteristics of the Planets
Graphics display of the J2000 heliocentric orbital characteristics of the solar system planets.

etwa ein Jahr vor | 2 Downloads |

0.0 / 5

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

etwa ein Jahr vor | 1 Download |

0.0 / 5

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

etwa ein Jahr vor | 2 Downloads |

0.0 / 5

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Modeling Orbital Maneuvers with MATLAB
Seven MATLAB scripts for modeling impulsive and finite-burn orbital maneuvers

etwa ein Jahr vor | 9 Downloads |

0.0 / 5

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Trans-Earth Trajectory Correction Maneuver – OTB
Optimize a single impulsive trajectory correction maneuver (TCM) on a trans-Earth (Moon-to-Earth) trajectory.

mehr als ein Jahr vor | 1 Download |

0.0 / 5

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Trans-Earth Trajectory Correction Maneuver - SNOPT
Optimize a single trans-Earth (Moon-to-Earth) impulsive trajectory correction maneuver (TCM). Target to entry interface (EI) or...

mehr als ein Jahr vor | 1 Download |

0.0 / 5

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

mehr als ein Jahr vor | 8 Downloads |

0.0 / 5

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N-body Lunar Free Return Trajectory Analysis – SNOPT
design an n-body, gravity-perturbed lunar free-return transfer trajectory from a circular Earth orbit to a final user-defined Ea...

mehr als ein Jahr vor | 2 Downloads |

0.0 / 5

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N-body Lunar Free Return Trajectory Analysis – OTB
Design and optimization of lunar free-return trajectories. Target to a final mission orbit or entry interface at Earth.

mehr als ein Jahr vor | 2 Downloads |

0.0 / 5

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Finite-burn De-orbit from Earth Orbit – SNOPT
Optimize a finite-burn maneuver that de-orbits a spacecraft from an initial circular or elliptical Earth orbit to a user-defined...

mehr als ein Jahr vor | 1 Download |

0.0 / 5

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Finite-burn raise of a circular or elliptical orbit - OTB
This script can be used to model a finite-burn maneuver that raises the perigee or apogee of an initial circular or elliptical o...

mehr als ein Jahr vor | 1 Download |

0.0 / 5

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Finite-burn lower of a circular or elliptical orbit - OTB
This script can be used to model a finite-burn maneuver that lowers the perigee or apogee of an initial circular or elliptical o...

mehr als ein Jahr vor | 1 Download |

0.0 / 5

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Finite-burn circularization of an elliptical orbit - OTB
This script circularizes an initial elliptical orbit by performing a finite-burn maneuver at apogee of the initial elliptical or...

mehr als ein Jahr vor | 1 Download |

0.0 / 5

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Finite-burn raise of a circular or elliptical orbit - SNOPT
This script can be used to model a finite-burn maneuver that raises the perigee or apogee of an initial circular or elliptical o...

mehr als ein Jahr vor | 2 Downloads |

0.0 / 5

Gesendet

Finite-burn lower of a circular or elliptical orbit - SNOPT
This script can be used to model a finite-burn maneuver that lowers the perigee or apogee of an initial circular or elliptical o...

mehr als ein Jahr vor | 1 Download |

0.0 / 5

Gesendet

Finite-burn circularization of an elliptical orbit - SNOPT
This script circularizes an initial elliptical orbit by performing a finite-burn maneuver at apogee of the initial elliptical or...

mehr als ein Jahr vor | 1 Download |

0.0 / 5

Gesendet

Parametric Analysis of TLI Delta-V Lunar Trajectories - OTB
Optimization Toolbox version of the tli_sweep MATLAB script that performs a parametric sweep of TLI requirements for Lunar traje...

fast 2 Jahre vor | 2 Downloads |

0.0 / 5

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Gravity Perturbed Optimal Orbital Transfer Analysis - SNOPT
Optimal two impulse transfer subject to non-spherical gravity perturbations

fast 2 Jahre vor | 1 Download |

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Gravity Perturbed Optimal Orbital Transfer Analysis - OTB
Optimal two impulse transfer subject to non-spherical gravity perturbations - Optimization Toolbox version

fast 2 Jahre vor | 2 Downloads |

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Computer Methods for Aerospace Trajectory Optimization
Additional technical documentation for the Orbital Mechanics with MATLAB scripts posted on the Mathworks File Exchange.

etwa 2 Jahre vor | 4 Downloads |

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MATLAB functions for solving Lambert's problem
Three MATLAB functions and a script that demonstrates how to interact with each Lambert routine.

etwa 2 Jahre vor | 4 Downloads |

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Gravity-Assist with a Powered Flyby - OTB version
MATLAB script that can be used to design and optimize interplanetary trajectories that include a powered flyby gravity assist.

etwa 2 Jahre vor | 1 Download |

0.0 / 5

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Gravity-Assist with a Powered Flyby - SNOPT version
MATLAB script that can be used to design and optimize interplanetary trajectories that include a powered gravity assist.

etwa 2 Jahre vor | 2 Downloads |

0.0 / 5

Gesendet

Parametric Analysis of TLI Delta-V Lunar Transfer
Parametric Analysis of Minimum TLI Delta-V Lunar Transfer Trajectories

etwa 2 Jahre vor | 2 Downloads |

0.0 / 5

Gesendet

A MATLAB Script for Predicting Equinoxes and Solstices
Predict the calendar date & UTC time of the equinoxes and solstices for a user-defined calendar year

mehr als 2 Jahre vor | 1 Download |

0.0 / 5

Gesendet

Propagating Interplanetary Trajectories from Earth to Mars
Numerically integrate the orbital equations of motion of an Earth to Mars interplanetary trajectory.

fast 3 Jahre vor | 5 Downloads |

5.0 / 5