Satellite Orbit Determination
Beschrijving
Course contents
1 Dynamics
Introduction to dynamics
Planetary Gravity field
Tides and the three-body problem
Hill radius and Roche limit
Relation to planetary sciences and astrodynamics
Solving Equations of motion
Reformulate orbit problem as a system of ordinary differential equations
Efficiency and accuracy of numerical integration methods
Implementation of numerical integration methods
2 Observations techniques and reference systems
Observation techniques
Laser, Doppler, optical and VLBI observations
Refraction, Electromagnetism, radio- and optical technology
Tropospheric and ionospheric refraction
Relativity and the definition of time,
Classification of time systems (UTC, TAI, etc)
Light-time effect
Quality of clocks (Allan Variance behavior of clocks)
Coordinate reference systems
Local and global coordinate systems
Definition of geoid and reference ellipsoid, height systems
Precession and nutation, polar motion, polar wander.
Newton or Einstein, consequences for reference systems
3 Statistics
Random variables, probability density functions, moments, hypothesis testing
Least squares minimization
Unconstrained linear parameter estimation,
Data weighting
Nonlinear parameter estimation.
Rank deficient equation systems
Singular value decomposition and Empirical Orthogonal functions
Penrose Moore inverse
Compatibility conditions
General and homogeneous solutions
Constrained linear parameter estimation
Mechanization of parameter estimation algorithms
Choice of algorithms
4 Orbit determination
Perturbation analysis and variational problems
State transition matrix for initial state vector problems
Partial derivatives for dynamical parameters
Parameter estimation
Identification of parameters
Batch least squares
Sequential least squares: The Kalman filter, theory and implementation
5 Applications
Global Navigation Satellite Systems:
Technology and terminology,
Various data processing strategies and available software
Modeling deformation of the solid Earth,
The Earth's gravity field and thermospheric density
Satellite laser ranging and Doppler tracking via DORIS
Technology and terminology, results and applications
Observing changes in the cryosphere with satellites
Hydrology and Oceanography observed with satellites
6 Individual assignments in quarter 2
The assignments will be announced during the quarter and typically take the following form
One test-your-knowledge exercise related to dynamics, observation systems or reference systems
A graded assignment related to GNSS applied to orbit determination
A graded assignment related to batch or sequential least squares methods
7 Numerical Practical in quarter 3
Exercises with the Ghost software, typical examples are to solve:
Initial value problems (state vector estimation)
Problems with parameters in a dynamic model (drag parameter estimation)
Problems with time bias parameters
Toetsing
The final grade will come together from:
Written examination resulting in a grade
Nominally two individual assignments resulting in a weighted average grade
Numerical practical resulting in "pass" or "fail".
The grading rules are as follows:
The numerical practical result should be: "pass"
The written examination result should be at least a 5,0
In order to participate in the numerical practical you must have passed the individual assignments with at least a weighted average of 5,0
No claims can be made with regard to individual assignment results or numerical practical results obtained before the previous academic year. For ae4-872 in 2025-2026 it means that results from 2024-2025 are still accepted, however, we do not accept results from 2023-2024 or earlier academic years. (Academic years run from September to August)
Due to the master curriculum refresh it is expected that ae4-872 orbit determination will run for the last time in academic year 2025-2026. This means that all course elements (exams, assignments and numerical practical) should be completed by the students in academic year 2025-2026.
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