photo

Meysam Mahooti


University of Tehran

Attivo dal 2016

Followers: 16   Following: 0

Messaggio

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

Statistica

All
  • Explorer
  • Knowledgeable Level 2
  • Personal Best Downloads Level 5
  • Editor's Pick
  • First Review
  • 5-Star Galaxy Level 5
  • First Submission
  • Revival Level 4
  • 3 Month Streak
  • First Answer

Visualizza badge

Feeds

Visto da

Inviato


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

circa 2 ore fa | 911 download |

Thumbnail

Inviato


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

circa 23 ore fa | 51 download |

Thumbnail

Inviato


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

3 mesi fa | 19 download |

Thumbnail

Inviato


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

3 mesi fa | 15 download |

Thumbnail

Inviato


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

3 mesi fa | 5 download |

Inviato


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

3 mesi fa | 8 download |

Thumbnail

Inviato


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

3 mesi fa | 22 download |

Thumbnail

Inviato


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

3 mesi fa | 17 download |

Thumbnail

Inviato


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

6 mesi fa | 7 download |

Thumbnail

Inviato


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

6 mesi fa | 6 download |

Inviato


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

6 mesi fa | 33 download |

Thumbnail

Inviato


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

6 mesi fa | 74 download |

Thumbnail

Inviato


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

7 mesi fa | 5 download |

Thumbnail

Inviato


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

7 mesi fa | 6 download |

Thumbnail

Inviato


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

8 mesi fa | 4 download |

Thumbnail

Inviato


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

9 mesi fa | 14 download |

Thumbnail

Inviato


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

9 mesi fa | 12 download |

Thumbnail

Inviato


NASA JPL Development Ephemerides (DE440)
High precision planetary ephemerides

10 mesi fa | 5 download |

Thumbnail

Inviato


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

11 mesi fa | 13 download |

Thumbnail

Inviato


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

12 mesi fa | 17 download |

Thumbnail

Inviato


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

circa un anno fa | 3 download |

Thumbnail

Inviato


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

circa un anno fa | 5 download |

Thumbnail

Inviato


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

circa un anno fa | 16 download |

Thumbnail

Inviato


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

circa un anno fa | 2 download |

Inviato


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

circa un anno fa | 12 download |

Inviato


SGP4/SDP4
SGP4 and SDP4 orbit propagators

circa un anno fa | 12 download |

Thumbnail

Inviato


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

circa un anno fa | 87 download |

Thumbnail

Inviato


Moon Phases
Determination of lunar phases and checking for eclipses

oltre un anno fa | 11 download |

Thumbnail

Inviato


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

oltre un anno fa | 2 download |

Thumbnail

Inviato


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

oltre un anno fa | 2 download |

Thumbnail

Carica altro