Control of Nonlinear Spacecraft Attitude Motion
Completed by Aaditya Sahoo
July 2, 2026
31 hours (approximately)
Aaditya Sahoo's account is verified. Coursera certifies their successful completion of Control of Nonlinear Spacecraft Attitude Motion
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
Skills you will gain
- Category: Mathematical Modeling
- Category: Differential Equations
- Category: Mechanics
- Category: Applied Mathematics
- Category: Engineering Analysis
- Category: Linear Algebra
- Category: Control Systems
- Category: Torque (Physics)
- Category: Numerical Analysis
