Course

Advanced Capstone Spacecraft Dynamics and Control Project

University of Colorado Boulder

This advanced capstone course, the final segment of the Advanced Spacecraft Dynamics and Control specialization, delves into the intricate dynamics of spacecraft systems with a focus on a spacecraft with a hinged panel. The course assumes prior completion of "Attitude Control with Momentum Exchange Devices" and "Analytical Mechanics for Spacecraft Dynamics". The curriculum is designed to provide comprehensive insights into the three-dimensional kinematics of the system, analytical relationships of body and panel position and velocity states, and the center of mass properties. Additionally, participants will explore the application of Lagrange's equations of motion to predict the dynamical response of a simplified system, and investigate the rotational response when applying attitude control torques to the spacecraft hub with a spring-hinged panel.

  • Learn to create and validate a simulation of a spacecraft with a hinged panel.
  • Investigate spacecraft dynamics with a time-varying geometry.

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Advanced Capstone Spacecraft Dynamics and Control Project
Course Modules

This course is divided into modules covering an introduction to the capstone project, exploration of the 3D spacecraft hub-panel system, and planar rotation control using bang-bang and filtered control solutions.

Introduction to the Capstone Project

Welcome to the Course! This module provides an overview of the capstone project, setting the stage for the comprehensive exploration of spacecraft dynamics and control.

3D Spacecraft Hub-Panel System

The 3D Spacecraft Hub-Panel System module delves into the intricacies of spacecraft dynamics, focusing on a system with a hinged panel. Participants will explore the three-dimensional kinematics of the system and derive analytical relationships of body and panel position and velocity states.

Planar Rotation Control using Bang-Bang and Filtered Control Solutions

The Planar Rotation Control module investigates the application of open-loop control torque solutions, specifically focusing on bang-bang and filtered control solutions for planar rotation. Participants will gain insights into the dynamical response and the impact of these control solutions on spacecraft dynamics.

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