Meysam Mahooti
University of Tehran
自 2016 起处于活动状态
I am a consultant for projects related to my file exchange source code. You can reach me at mahooti007@gmail.com.
Programming Languages:
C++, C, MATLAB
Spoken Languages:
English
Professional Interests:
Numerical Integration and Differential Equations, Least Squares, Aerospace and Defense, Satellite and Orbital Mechanics
C++, C, MATLAB
Spoken Languages:
English
Professional Interests:
Numerical Integration and Differential Equations, Least Squares, Aerospace and Defense, Satellite and Orbital Mechanics
Feeds
已提交
Relay Satellite Orbit Determination
Orbit Determination from Tracking and Data Relay Satellite Measurements
2 months 前 | 7 次下载 |
已提交
Real-Time Orbit Determination
Real-Time Orbit Determination based on GPS Navigation Data
2 months 前 | 9 次下载 |
已提交
Satellite Orbit Modeling
Precise modeling of satellite's perturbed motion (special perturbations approach)
2 months 前 | 11 次下载 |
已提交
Satellite Orbits: Models, Methods and Applications
Satellite Orbits: Models, Methods and Applications
2 months 前 | 31 次下载 |
已提交
High Precision Orbit Propagator
Precise modeling of satellite's perturbed motion (special perturbations approach)
2 months 前 | 23 次下载 |
已提交
Initial Orbit Determination (Angles-Only Method)
Angles-only approach applying the Least Squares method
6 months 前 | 9 次下载 |
已提交
Initial Orbit Determination (Extended Kalman Filter)
Initial orbit determination applying the Extended Kalman Filter
6 months 前 | 9 次下载 |
已提交
Initial Orbit Determination (Least Squares Method)
Initial orbit determination applying the Least Squares method
6 months 前 | 11 次下载 |
已提交
Local Circumstances of a Solar Eclipse
Computation of possibility of observing solar eclipse at the observer's location
6 months 前 | 2 次下载 |
已提交
Solar Eclipse
Prediction of solar eclipse and its duration using the time of new moon
6 months 前 | 4 次下载 |
已提交
ECI2ECEF & ECEF2ECI Transformations
The transformation from celestial to terrestrial reference system and vice versa
6 months 前 | 11 次下载 |
已提交
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
9 months 前 | 4 次下载 |
已提交
Jacchia-Bowman Atmospheric Density Model
Computation of the total mass density of the atmosphere using the Jacchia-Bowman model
9 months 前 | 15 次下载 |
已提交
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).
9 months 前 | 6 次下载 |
已提交
NRLMSISE-00 Atmosphere Model
Computation of neutral temperature and densities in Earth's atmosphere from ground to thermospheric heights.
10 months 前 | 23 次下载 |
已提交
SGP8
The SGP8 model to calculate orbital state vectors of near-Earth satellites
1 year 前 | 6 次下载 |
已提交
Sun Position (VSOP87)
VSOP87 defines the analytical solutions to the motions of the solar system planets
1 year 前 | 5 次下载 |
已提交
Moon Position
Position of the Moon referred to the mean equator and equinox of J2000
1 year 前 | 6 次下载 |
已提交
Sun Position
Geocentric equatorial position of the Sun (in [m]), referred to the ICRF
1 year 前 | 10 次下载 |
已提交
Satellite Visibility
Propagation of the satellite's state vector using SGP4 and checking its visibility for future
1 year 前 | 9 次下载 |
已提交
NASA JPL Development Ephemerides (DE405)
DE405 covers 1599-12-09 to 2201-02-20. Referred to the International Celestial Reference Frame.
1 year 前 | 10 次下载 |
已提交
Initial orbit determination
Initial orbit determination (two sets of range and angle measurements of a satellite)
1 year 前 | 5 次下载 |
已提交
NASA JPL Development Ephemerides (DE440)
High precision planetary ephemerides
1 year 前 | 2 次下载 |
已提交
NASA JPL Development Ephemerides (DE441)
High-precision computation of planetary ephemerides
1 year 前 | 6 次下载 |
已提交
Lambert's Problem
Lambert’s problem is the orbital boundary-value problem constrained by two points and elapsed time.
1 year 前 | 7 次下载 |
已提交
Sunrise Sunset
Rising and setting times of the Sun and the Moon and twilight times
2 years 前 | 5 次下载 |
