Control of Nonlinear Spacecraft Attitude Motion (Coursera)

Control of Nonlinear Spacecraft Attitude Motion (Coursera)

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Descripción de “Control of Nonlinear Spacecraft Attitude Motion (Coursera)”

This course trains you in the skills needed to program specific orientation and achieve precise aiming goals for spacecraft moving through three dimensional space. First, we cover stability definitions of nonlinear dynamical systems, covering the difference between local and global stability. We then analyze and apply Lyapunov’s Direct Method to prove these stability properties, and develop a nonlinear 3-axis attitude pointing control law using Lyapunov theory. Finally, we look at alternate feedback control laws and closed loop dynamics.

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

Who is this class for: This class is for working engineering professionals looking to add to their skill sets, graduate students in engineering looking to fill gaps in their knowledge base, and enterprising engineering undergraduates looking to expand their horizons.

Syllabus

WEEK 1

Nonlinear Stability Definitions

Discusses stability definitions of nonlinear dynamical systems, and compares to the classical linear stability definitions. The difference between local and global stability is covered.

Graded: Concept Check 1 – State Vector Representation

Graded: Concept Check 2 – State Neighborhood

Graded: Concept Check 3 – Lagrange Stability

Graded: Concept Check 4 – Lyapunov Stability

Graded: Concept Check 5 – Asymptotic Stability

Graded: Concept Check 6 – Global Stability Definitions

Graded: Concept Check 7 – Linearization

WEEK 2

Overview of Lyapunov Stability Theory

Lyapunov’s direct method is employed to prove these stability properties for a nonlinear system and prove stability and convergence. The possible function definiteness is introduced which forms the building block of Lyapunov’s direct method. Convenient prototype Lyapunov candidate functions are presented for rate- and state-error measures.

Graded: Concept Check 1 – Definite Function

Graded: Concept Check 2 – Lyapunov Functions

Graded: Concept Check 3 – Asymptotic Stability

Graded: Concept Check 4 – Global Stability Applications

Graded: Concept Check 5 – General Elemental Rate

Graded: Concept Check 6 – Rigid Body Elemental Rate Lyapunov Function

Graded: Concept Check 7 – General Elemental State Lyapunov Function

WEEK 3

Attitude Control of States and Rates

A nonlinear 3-axis attitude pointing control law is developed and its stability is analyized using Lyapunov theory. Convergence is discussed considering both modeled and unmodeled torques. The control gain selection is presented using the convenient linearized closed loop dynamics.

Graded: Concept Check 1 – General 3-Axis Attitude Control

Graded: Concept Check 2 – Asymptotic Stability

Graded: Concept Check 3 – Unknown External Torques

Graded: Concept Check 4 – Integral Feedback

Graded: Concept Check 5 – Feedback Gain Selection

WEEK 4

Alternate Attitude Control Formulations

Alternate feedback control laws are formulated where actuator saturation is considered. Further, a control law is presented that perfectly linearizes the closed loop dynamics in terms of quaternions and MRPs. Finally, the 3-axis Lyapunov attitude control is developed for a spacecraft with a cluster of N reaction wheel control devices.

Graded: Concept Check 1 – Saturated Control

Graded: Concept Check 2 – Linearized Closed Loop Dynamics

Graded: Concept Check 3 – RW Feedback Control

Graded: Nonlinear Control Final Assignment

Especificaciones: Control of Nonlinear Spacecraft Attitude Motion (Coursera)

Curso ofrecido por
Disponibilidad

✔ Disponible

Plataforma

Universidad

Impartido por

Hanspeter Schaub

País

USA

Nivel, duración y fechas
Nivel

Avanzado

Fecha

04/05/2020

Duración

4 semanas

Tiempo necesario

2-5 horas/semana

Idioma del curso
Idioma vehicular

Inglés

Subtítulos

No informado

Exámenes y Certificados
Certificados

Certificado de Pago

Exámenes/Proyectos

Con Examen/Proyecto Final de pago

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Control of Nonlinear Spacecraft Attitude Motion (Coursera)
Control of Nonlinear Spacecraft Attitude Motion (Coursera)

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