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Meysam Mahooti


University of Tehran

Attivo dal 2016

Followers: 0   Following: 0

Contatto

Programming Languages:
MATLAB
Spoken Languages:
English
Professional Interests:
Numerical Integration and Differential Equations, Aerospace, Satellite and Orbital Mechanics

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NASA JPL Development Ephemerides (DE405)
DE405 covers 1599-12-09 to 2201-02-20. Referred to the International Celestial Reference Frame.

4 giorni fa | 28 download |

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Initial orbit determination
Initial orbit determination (two sets of range and angle measurements of a satellite)

12 giorni fa | 9 download |

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Satellite Visibility
Propagation of the satellite's state vector using SGP4 and checking its visibility for future

13 giorni fa | 14 download |

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Initial Orbit Determination (Least Squares Method)
Initial orbit determination applying the Least Squares method

circa 2 mesi fa | 24 download |

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Initial Orbit Determination (Angles-Only Method)
Angles-only approach applying the Least Squares method

circa 2 mesi fa | 14 download |

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NASA JPL Development Ephemerides (DE440)
High precision planetary ephemerides

2 mesi fa | 9 download |

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NASA JPL Development Ephemerides (DE441)
High-precision computation of planetary ephemerides

4 mesi fa | 15 download |

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Lambert's Problem
Lambert’s problem is the orbital boundary-value problem constrained by two points and elapsed time.

4 mesi fa | 18 download |

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ECEF2ECI & ECI2ECEF Transformations_IAU 2006 Resolutions
Transformation from terrestrial to celestial reference system and vice versa

7 mesi fa | 6 download |

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ECI2ECEF & ECEF2ECI Transformations
Transformation from celestial to terrestrial reference system and vice versa

7 mesi fa | 30 download |

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Sunrise Sunset
Rising and setting times of the Sun and the Moon and twilight times

7 mesi fa | 5 download |

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Sunrise Sunset
Rising and setting times of the Sun and the Moon and twilight times

7 mesi fa | 7 download |

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Initial Orbit Determination (Extended Kalman Filter)
Initial orbit determination applying the Extended Kalman Filter

7 mesi fa | 13 download |

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Double-r Initial Orbit Determination
Double-r method is utilized to determine the initial orbit.

8 mesi fa | 5 download |

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Gauss Initial Orbit Determination
Gauss's method is utilized to determine the initial orbit.

8 mesi fa | 9 download |

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SGP4/SDP4
SGP4 and SDP4 orbit propagators

8 mesi fa | 20 download |

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SGP4
The SGP4 model to calculate orbital state vectors of near-Earth satellites

8 mesi fa | 77 download |

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High Precision Orbit Propagator
Precise modeling of satellite's perturbed motion (special perturbations approach)

8 mesi fa | 78 download |

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Satellite Orbit Modeling
Modeling of satellite's perturbed motion (special perturbations approach)

8 mesi fa | 32 download |

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Moon Phases
Determination of lunar phases and checking for eclipses

9 mesi fa | 6 download |

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JPL Development Ephemerides
Computation of position and velocity of major planets, the Moon, and the Sun

11 mesi fa | 2 download |

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Solar Eclipse
Prediction of solar eclipse and its duration using the time of new moon

11 mesi fa | 20 download |

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Moon Age
Computation of the Moon age and its phase

11 mesi fa | 5 download |

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Jacchia-Bowman Atmospheric Density Model
Computation of the total mass-desnity of atmosphere using Jacchia-Bowman model

oltre un anno fa | 15 download |

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Modified Jacchia 70
Computation of atmospheric density for drag effect modeling

oltre un anno fa | 5 download |

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Sun/Moon Rise/Set
Rising and setting times of the Sun and the Moon and twilight times

oltre un anno fa | 4 download |

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Local Circumstances of a Solar Eclipse
Computation of possibility of observing solar eclipse at the observer's location

oltre un anno fa | 4 download |

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Moon Position
Position of the Moon referred to the mean equator and equinox of J2000

oltre un anno fa | 15 download |

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Sun Position (VSOP87)
VSOP87 defines the analytical solutions to the motions of the solar system planets

oltre un anno fa | 5 download |

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Sun Position
Geocentric equatorial position of the Sun (in [m]), referred to the ICRF

oltre un anno fa | 16 download |

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