Control of Nonlinear Spacecraft Attitude Motion
Completed by Vikash Kumar Jaiswal
September 21, 2020
31 hours (approximately)
Vikash Kumar Jaiswal'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: Engineering Analysis
- Category: Mathematical Modeling
- Category: Systems Analysis
- Category: Linear Algebra
- Category: Torque (Physics)
- Category: Mechanics
- Category: Differential Equations
- Category: Control Systems
- Category: Applied Mathematics
