Near Real-Time Closed-Loop Optimal Control Feedback for Spacecraft Attitude Maneuvers

By C. McFarland

Optimization of spacecraft attitude maneuvers can significantly reduce attitude control system size and mass, and extend satellite end-of-life. Optimal control theory has been applied to solve a... This description may be from another edition of this product.

• Format: Paperback
• Language: English
• ISBN: 1288331436
• ISBN13: 9781288331437
• Release Date: November 2012
• Publisher: Biblioscholar
• Length: 152 Pages
• Weight: 0.63 lbs.
• Dimensions: 0.3" x 7.4" x 9.7"