Attitude Control with Momentum Exchange Devices (Coursera)

The course discusses developing a complex spacecraft simulation with a number VSCMGs and how to approach debugging such complex software. The use of the work/energy theorem is discussed to assist with debugging the simulation by validating angular momentum, energy, changes in momentum and mechanical power.

Further, the use of null motion is explored to reconfigure the attitude control devices to avoid singularities and gimbal lock. The redundancy is exploited to seek control solutions that avoid classical CMG singularities.
What You Will Learn

- D​eveloping spacecraft equations of motion with momentum exchange devices

- W​riting and validating complex spacecraft simulations

- E​xploiting momentum device nullmotion to avoid singularities.

Syllabus

WEEK 1

Revisiting Basics of Spacecraft Kinematics

The prerequisite topics of spacecraft kinematics are reviewed in this module. This sequence is intended to ramp up the student on the mathematical tools and concepts required for this course. For each topic we also dig a little deeper into the subject matter.

WEEK 2

Revisiting Basics of Spacecraft Kinetics

Review of fundamental properties of a closed dynamical system leading to the development of the equations of motion.

WEEK 3

Revisiting the Basics of Nonlinear Spacecraft Control

Review of the fundamental nonlinear stability definitions, using Lyapunov's direct method, as well as discussing stability proof modifications if the system is time dependent.

WEEK 4

VSCMG Dynamics

Develop the kinematics and kinetics of the variable speed CMG devices.

WEEK 5

Momentum Based 3-Axis Attitude Control

Learn how to achieve 3-axis attitude feedback control using a series of momentum exchange devices such as reaction wheels, control moment gyroscopes (CMGs) and variable speed CMGs