Satellite Orbits: Models, Methods and Applications
Exercise 2-1: Orbit raising using Hohmann transfer
Exercise 2-2: Solution of Kepler's equation
Exercise 2-3: Osculating elements
Exercise 2-4: Topocentric satellite motion
Exercise 2-5: Sunsynchronous repeat orbits
Exercise 2-6: Initial orbit determination (two sets of range and angle measurements of a satellite)
Exercise 3-1: Gravity field
Exercise 3-2: Lunar ephemerides
Exercise 3-3: Accelerations
Exercise 3-4: Orbit Perturbations
Exercise 4-1: Runge-Kutta 4th-order Integration
Exercise 4-2: Gauss-Jackson 4th-order predictor
Exercise 4-3: Step size control of DE multistep method
Exercise 5-1: Transformation from celestial to terrestrial reference system
Exercise 5-2: Velocity in the Earth-fixed frame
Exercise 5-3: Geodetic coordinates
Exercise 6-1: Light Time Iteration
Exercise 6-2: Range Rate Modelling
Exercise 6-3: User Clock Error from GPS Pseudorange
Exercise 6-4: Tropospheric Refraction
Exercise 7-1: State transition matrix
Exercise 8-1: Least-squares fit using Givens rotations
Exercise 8-2: Least-squares orbit determination
Exercise 8-3: Orbit Determination using Extended Kalman Filter
GEODA : Geostationary satellite Orbit Determination error Analysis
RTOD : Real Time Orbit Determination based on GPS navigation data
TDRSOD : Orbit Determination from Tracking and Data Relay Satellite measurements
Reference:
O. Montenbruck, E. Gill, "Satellite Orbits: Models, Methods and Applications", Springer Verlag, Heidelberg, 2005.
引用格式
Meysam Mahooti (2024). Satellite Orbits: Models, Methods and Applications (https://www.mathworks.com/matlabcentral/fileexchange/54840-satellite-orbits-models-methods-and-applications), MATLAB Central File Exchange. 检索来源 .
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- Industries > Aerospace and Defense > CubeSat and Satellites >
- Sciences > Physics > Gravitation, Cosmology & Astrophysics >
- Aerospace and Defense > Aerospace Blockset > Reference Applications >
- Engineering > Aerospace Engineering > Satellite and Orbital Mechanics >
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版本 | 已发布 | 发行说明 | |
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1.0.0.0 | TDRSOD.m and Trj.m are changed to decrease the CPU time.
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