Meysam Mahooti
University of Tehran
MATLAB
Spoken Languages:
English
Professional Interests:
Numerical Integration and Differential Equations, Least Squares, Aerospace and Defense, Satellite and Orbital Mechanics
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Feeds
제출됨
Runge-Kutta-Fehlberg (RKF78)
Fehlberg's 7th and 8th Order Embedded Method
대략 4시간 전 | 다운로드 수: 911 |
제출됨
NRLMSISE-00 Atmosphere Model
Computation of neutral temperature and densities in Earth's atmosphere from ground to thermospheric heights.
1일 전 | 다운로드 수: 51 |
제출됨
Real-Time Orbit Determination
Real-Time Orbit Determination based on GPS Navigation Data
3개월 전 | 다운로드 수: 19 |
제출됨
SGP8
The SGP8 model to calculate orbital state vectors of near-Earth satellites
3개월 전 | 다운로드 수: 15 |
제출됨
Sun Position (VSOP87)
VSOP87 defines the analytical solutions to the motions of the solar system planets
3개월 전 | 다운로드 수: 5 |
제출됨
Moon Position
Position of the Moon referred to the mean equator and equinox of J2000
3개월 전 | 다운로드 수: 8 |
제출됨
ECI2ECEF & ECEF2ECI Transformations
The transformation from celestial to terrestrial reference system and vice versa
3개월 전 | 다운로드 수: 22 |
제출됨
Sun Position
Geocentric equatorial position of the Sun (in [m]), referred to the ICRF
3개월 전 | 다운로드 수: 17 |
제출됨
Relay Satellite Orbit Determination
Orbit Determination from Tracking and Data Relay Satellite Measurements
6개월 전 | 다운로드 수: 7 |
제출됨
Satellite Orbit Modeling
Modeling of satellite's perturbed motion (special perturbations approach)
6개월 전 | 다운로드 수: 33 |
제출됨
High Precision Orbit Propagator
Precise modeling of satellite's perturbed motion (special perturbations approach)
6개월 전 | 다운로드 수: 74 |
제출됨
Satellite Visibility
Propagation of the satellite's state vector using SGP4 and checking its visibility for future
7개월 전 | 다운로드 수: 5 |
제출됨
NASA JPL Development Ephemerides (DE405)
DE405 covers 1599-12-09 to 2201-02-20. Referred to the International Celestial Reference Frame.
7개월 전 | 다운로드 수: 6 |
제출됨
Initial orbit determination
Initial orbit determination (two sets of range and angle measurements of a satellite)
8개월 전 | 다운로드 수: 4 |
제출됨
Initial Orbit Determination (Least Squares Method)
Initial orbit determination applying the Least Squares method
9개월 전 | 다운로드 수: 14 |
제출됨
Initial Orbit Determination (Angles-Only Method)
Angles-only approach applying the Least Squares method
9개월 전 | 다운로드 수: 12 |
제출됨
NASA JPL Development Ephemerides (DE440)
High precision planetary ephemerides
10개월 전 | 다운로드 수: 5 |
제출됨
NASA JPL Development Ephemerides (DE441)
High-precision computation of planetary ephemerides
11개월 전 | 다운로드 수: 13 |
제출됨
Lambert's Problem
Lambert’s problem is the orbital boundary-value problem constrained by two points and elapsed time.
12개월 전 | 다운로드 수: 17 |
제출됨
Sunrise Sunset
Rising and setting times of the Sun and the Moon and twilight times
대략 1년 전 | 다운로드 수: 3 |
제출됨
Sunrise Sunset
Rising and setting times of the Sun and the Moon and twilight times
대략 1년 전 | 다운로드 수: 5 |
제출됨
Initial Orbit Determination (Extended Kalman Filter)
Initial orbit determination applying the Extended Kalman Filter
대략 1년 전 | 다운로드 수: 16 |
제출됨
Double-r Initial Orbit Determination
Double-r method is utilized to determine the initial orbit.
대략 1년 전 | 다운로드 수: 2 |
제출됨
Gauss Initial Orbit Determination
Gauss's method is utilized to determine the initial orbit.
대략 1년 전 | 다운로드 수: 12 |
제출됨
SGP4
The SGP4 model to calculate orbital state vectors of near-Earth satellites
대략 1년 전 | 다운로드 수: 87 |
제출됨
JPL Development Ephemerides
Computation of position and velocity of major planets, the Moon, and the Sun
1년 초과 전 | 다운로드 수: 2 |
제출됨
Solar Eclipse
Prediction of solar eclipse and its duration using the time of new moon
1년 초과 전 | 다운로드 수: 2 |
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