A Neural Network Approach to Fault Detection in Spacecraft Attitude Determination and Control Systems

This thesis proposes a method of performing fault detection and isolation in spacecraft attitude determination and control systems. The proposed method works by deploying a trained neural network to analyze a set of residuals that are dened such that they encompass the attitude control, guidance, an...

Full description

Bibliographic Details
Main Author: Schreiner, John N.
Format: Others
Published: DigitalCommons@USU 2015
Subjects:
Online Access:https://digitalcommons.usu.edu/etd/4164
https://digitalcommons.usu.edu/cgi/viewcontent.cgi?article=5181&context=etd