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
Other Authors: Sands, Timothy (Editor)
Format: Electronic Book Chapter
Language:English
Published: InTechOpen 2020
Subjects:
Online Access:OAPEN Library: download the publication
OAPEN Library: description of the publication
Tags: Add Tag
No Tags, Be the first to tag this record!