Meysam Mahooti - MATLAB Central
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Meysam Mahooti


University of Tehran

Attivo dal 2016

Followers: 20   Following: 0

Messaggio

I am a consultant for projects related to my file exchange source code. You can reach me at mahooti007@gmail.com.

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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Inviato


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

4 giorni fa | 24 download |

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

4 giorni fa | 71 download |

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

4 giorni fa | 14 download |

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

5 giorni fa | 10 download |

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

6 giorni fa | 34 download |

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

circa un mese fa | 12 download |

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

circa un mese fa | 15 download |

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Satellite Orbits: Models, Methods and Applications
Satellite Orbits: Models, Methods and Applications

2 mesi fa | 37 download |

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Positions of solar system bodies
The heliocentric and geocentric positions of the solar system's eight planets, in addition to the Moon and the Sun

2 mesi fa | 3 download |

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

3 mesi fa | 14 download |

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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).

3 mesi fa | 12 download |

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

3 mesi fa | 7 download |

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

3 mesi fa | 34 download |

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

6 mesi fa | 7 download |

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

6 mesi fa | 3 download |

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

6 mesi fa | 12 download |

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

6 mesi fa | 15 download |

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

9 mesi fa | 2 download |

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

10 mesi fa | 8 download |

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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.

11 mesi fa | 12 download |

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

11 mesi fa | 2 download |

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

12 mesi fa | 10 download |

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NASA JPL Development Ephemerides (DE440)
High precision planetary ephemerides

circa un anno fa | 6 download |

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

circa un anno fa | 11 download |

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

circa un anno fa | 11 download |

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

oltre un anno fa | 2 download |

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

oltre un anno fa | 1 download |

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

oltre un anno fa | 7 download |

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

oltre un anno fa | 9 download |

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SGP4/SDP4
SGP4 and SDP4 orbit propagators

oltre un anno fa | 17 download |

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