Control of Nonlinear Spacecraft Attitude Motion

This course is part of Spacecraft Dynamics and Control Specialization

Instructor: Hanspeter Schaub

What you'll 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
  • Skills you'll gain

  •   Engineering Analysis
  •   Applied Mathematics
  •   Control Systems
  •   Torque (Physics)
  •   Mechanics
  •   Differential Equations
  •   Vibrations
  •   Mathematical Modeling
  •   Simulation and Simulation Software
  • 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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