Community Profile

photo

Meysam Mahooti


celestrak.com

22 total contributions since 2016

Contact

Meysam Mahooti's Badges

  • 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

View details...

Contributions in
View by

Answered
Computation of GPS receiver position based on observation files
Initial guess of GPS receiver position is obtained from observation file and is updated using broadcast orbits, pseudorange and ...

1 dag ago | 0

Answered
computation of GPS receiver position based on RINEX observation file
Initial guess of GPS receiver position is obtained from observation file and is updated using broadcast orbits, pseudorange and ...

1 dag ago | 0

Submitted


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

3 dagen ago | 16 downloads |

Thumbnail

Submitted


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

5 dagen ago | 44 downloads |

Thumbnail

Submitted


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

14 dagen ago | 83 downloads |

Thumbnail

Answered
How would i convert latitude and longitude to meters from a point?
%-------------------------------------------------------------------------- % % Position: Position vector (r [m]) from geodeti...

17 dagen ago | 1

Answered
Geodetic to cartesian coordinates
%-------------------------------------------------------------------------- % % Position: Position vector (r [m]) from geodeti...

17 dagen ago | 0

Submitted


GPS Receiver Position
Computation of GPS receiver position based on navigation and observation files

17 dagen ago | 68 downloads |

Thumbnail

Answered
Coorindate transforms to a satellite reference frame
ECEF2ECI.m is one of the functions which is used in High Precision Orbit Propagator in the following link: https://www.mathwork...

24 dagen ago | 0

Answered
How to convert ECI coordinates with given sidereal time to ECEF coordinates ?
ECI2ECEF.m is one of the functions which is used in High Precision Orbit Propagator in the following link: https://www.mathwork...

ongeveer een maand ago | 0

Answered
how to draw a satellite ground track on top of a map
https://www.mathworks.com/matlabcentral/fileexchange/66000-groundtrack

ongeveer een maand ago | 0

Answered
Calculate sunrise and sunset time
https://www.mathworks.com/matlabcentral/fileexchange/60157-sunrise-sunset https://www.mathworks.com/matlabcentral/fileexchange/...

ongeveer 2 maanden ago | 0

Submitted


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

ongeveer 2 maanden ago | 52 downloads |

Thumbnail

Submitted


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

4 maanden ago | 16 downloads |

Thumbnail

Submitted


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

4 maanden ago | 37 downloads |

Thumbnail

Submitted


Runge Kutta 8th Order Integration
Runge-Kutta 8th order numerical integration method

7 maanden ago | 15 downloads |

Thumbnail

Submitted


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

8 maanden ago | 6 downloads |

Submitted


Moon Phases
Determination of lunar phases and checking for eclipses

8 maanden ago | 10 downloads |

Thumbnail

Submitted


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

8 maanden ago | 10 downloads |

Thumbnail

Submitted


Iinitial Orbit Determination (Angles-only Method)
orbit determination with differential correction

8 maanden ago | 9 downloads |

Thumbnail

Submitted


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

8 maanden ago | 17 downloads |

Thumbnail

Submitted


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

8 maanden ago | 9 downloads |

Thumbnail

Answered
Does anybody know how should I use animatedline in order to draw me an orbit immediately? (I have used drawnow and it doesn t work)
You can use my different orbit propagators which all of them draw satellite's groundtrack after finishing propagation: https://...

8 maanden ago | 1

Submitted


DOING PHYSICS WITH MATLAB
Matlab is a well suited tool for modeling the physical world and using it can be beneficial to students studying physics and eng...

9 maanden ago | 0 downloads |

Thumbnail

Submitted


Two Body Orbit Propagation (non-spherical Earth)
Satellite Gravity Field Missions: Simulation Scenarios

10 maanden ago | 13 downloads |

Thumbnail

Answered
Adams Bashforth Multon Code not running
https://ch.mathworks.com/matlabcentral/fileexchange/55433-adams-bashforth-moulton

11 maanden ago | 1

Answered
script or function for moon phase and position with time, lat and lon as inputs
https://www.mathworks.com/matlabcentral/fileexchange/56041-moon-position?s_tid=prof_contriblnk https://www.mathworks.com/matlabc...

11 maanden ago | 0

| accepted

Submitted


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

11 maanden ago | 54 downloads |

Thumbnail

Submitted


Adams-Bashforth-Moulton
Adams-Bashforth-Moulton integration (8th order)

11 maanden ago | 16 downloads |

Submitted


Runge Kutta 4th order
Classical 4th order Runge-Kutta method

11 maanden ago | 33 downloads |

Thumbnail

Load more