Stock Image

Robust Three-Axis Attitude Control System for Micro Satellites

Zizung Yoon

ISBN 10: 3844001344 / ISBN 13: 9783844001341
Published by Shaker Verlag Jun 2011, 2011
New Condition: Neu Soft cover
From Agrios-Buch (Bergisch Gladbach, Germany)

AbeBooks Seller Since 11 January 2012

Quantity Available: 1

Buy New
Price: £ 42.31 Convert Currency
Shipping: £ 15.36 From Germany to U.S.A. Destination, Rates & Speeds
Add to basket

About this Item

Neuware - Technical advances in microelectronics and micromechanics signalled the start of an era for small satellites in the late 1980's. Particularly in the last decade small satellites have proven their potential not only in missions with scientific and educational objectives, but also for those with cost-effective commercial and governmental purposes. Fault tolerance and reliability still remain however, a key issue for technical and economical advancement in small satellite design. This thesis therefore proposes a concept for a fault tolerant and robust attitude determination and control system adapted to micro satellites. After an investigation of modern fault handling approaches, a model based fault detection approach with hardware redundancy was chosen. This approach is particularly applicable for the use in small satellites, as the fault detection is realized not necessarily by additional hardware but by software algorithms. A hierarchical fault handling concept, a model based fault detection algorithm, and a novel time-optimal state control algorithm are all proposed. These algorithms were verified in a simulation and implemented in the three-axis attitude control system of the small satellite TET-1. Finally the concept was successfully verified in a hardware-in-the-loop test bed. The hierarchical fault handling and model based fault detection approach is also applicable for any other small satellite, for which dedicated fault handling hardware is not suitable due to cost, mass, or power limitations. The time-optimal attitude and rate control algorithm enable optimal attitude control performance in the presence of system noise. This thesis therefore provides a general methodology for the design of a reliable, fault-tolerant, and robust attitude control system for small (micro) satellites. 137 pp. Englisch. Bookseller Inventory # 9783844001341

Ask Seller a Question

Bibliographic Details

Title: Robust Three-Axis Attitude Control System ...

Publisher: Shaker Verlag Jun 2011

Publication Date: 2011

Binding: Taschenbuch

Book Condition:Neu

Store Description

Visit Seller's Storefront

Terms of Sale:

Allgemeine Geschäftsbedingungen (

der Firma Agrios Buch- und Medienversand UG e.K. ,Geschäftsführer Ludwig Meier, De-Gasperi-Str. 8, 51469 Bergisch Gladbach nachstehend als Verkäufer bezeichnet.

§ 1 Allgemeines, Begriffsbestimmungen

(1) Der Verkäufer bietet unter dem Nutzernamen Agrios Buch unter der Plattform insbesondere Bücher an. Die folgenden Allgemeinen Geschäftsbedingungen (AGB) gelten für die Geschäftsbeziehung zwischen dem Verkäufer und dem Kunden in ihrer zum Ze...

More Information
Shipping Terms:

Der Versand ins Ausland findet IMMER mit DHL statt. Auch nach Österreich verschicken wir nur mit DHL! Daher Standardversand == Luftpost!

Detailed Seller Information

List this Seller's Books

Payment Methods
accepted by seller

Visa Mastercard American Express

Check PayPal Invoice Bank/Wire Transfer