Control of Nonlinear Spacecraft Attitude Motion
This course is part of Spacecraft Dynamics and Control Specialization
Instructor: Hanspeter Schaub
What you'll learn
Skills you'll gain
There are 4 modules in this course
After this course, you will be able to... * Differentiate between a range of nonlinear stability concepts * Apply Lyapunov’s direct method to argue stability and convergence on a range of dynamical systems * Develop rate and attitude error measures for a 3-axis attitude control using Lyapunov theory * Analyze rigid body control convergence with unmodeled torque The material covered is taking from the book "Analytical Mechanics of Space Systems" available at https://arc.aiaa.org/doi/book/10.2514/4.105210.
Overview of Lyapunov Stability Theory
Attitude Control of States and Rates
Alternate Attitude Control Formulations
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