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Meysam Mahooti


University of Tehran

Active since 2016

Followers: 16   Following: 0

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

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  • Revival Level 4
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Submitted


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

5 days ago | 29 downloads |

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NASA JPL Development Ephemerides (DE430)
DE430 spans from 1549-12-21 to 2650-01-25 and is based on the International Celestial Reference Frame (version 2.0).

10 days ago | 16 downloads |

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Runge-Kutta-Fehlberg (RKF78)
Fehlberg's 7th and 8th Order Embedded Method

12 days ago | 12 downloads |

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NRLMSISE-00 Atmosphere Model
Computation of neutral temperature and densities in Earth's atmosphere from ground to thermospheric heights.

13 days ago | 52 downloads |

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Real-Time Orbit Determination
Real-Time Orbit Determination based on GPS Navigation Data

3 months ago | 15 downloads |

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SGP8
The SGP8 model to calculate orbital state vectors of near-Earth satellites

3 months ago | 14 downloads |

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

3 months ago | 5 downloads |

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

3 months ago | 9 downloads |

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

3 months ago | 16 downloads |

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

4 months ago | 10 downloads |

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Relay Satellite Orbit Determination
Orbit Determination from Tracking and Data Relay Satellite Measurements

6 months ago | 7 downloads |

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Radau IIA
Variable-order Radau IIA integrator with step-size control

6 months ago | 6 downloads |

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

7 months ago | 53 downloads |

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

8 months ago | 8 downloads |

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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.

8 months ago | 12 downloads |

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

8 months ago | 1 download |

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

9 months ago | 15 downloads |

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

9 months ago | 9 downloads |

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NASA JPL Development Ephemerides (DE440)
High precision planetary ephemerides

10 months ago | 5 downloads |

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

11 months ago | 13 downloads |

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

12 months ago | 19 downloads |

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

1 year ago | 4 downloads |

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

1 year ago | 5 downloads |

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

1 year ago | 15 downloads |

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

1 year ago | 2 downloads |

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

1 year ago | 16 downloads |

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SGP4/SDP4
SGP4 and SDP4 orbit propagators

1 year ago | 11 downloads |

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

1 year ago | 81 downloads |

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Moon Phases
Determination of lunar phases and checking for eclipses

1 year ago | 10 downloads |

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

1 year ago | 2 downloads |

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