Advances in Spacecraft Attitude Control

Spacecraft attitude maneuvers comply with Euler's moment equations, a set of three nonlinear, coupled differential equations. Nonlinearities complicate the mathematical treatment of the seemingly simple action of rotating, and these complications lead to a robust lineage of research. This book...

Full description

Saved in:
Bibliographic Details
Main Author: Timothy Sands (Author)
Format: Ebooks
Subjects:
Online Access:Get Fulltext
Tags: Add Tag
No Tags, Be the first to tag this record!

Similar Items