Control of Nonlinear Spacecraft Attitude Motion
Completed by RODRIGO NASCENTE SCHMITT
September 5, 2020
31 hours (approximately)
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What you will learn
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
