Spacecraft Dynamics and Control: An Introduction | Agenda Bookshop Skip to content
Please note that books with a 10-20 working days delivery time may not arrive before Christmas.
Please note that books with a 10-20 working days delivery time may not arrive before Christmas.
A01=Anton H. de Ruiter
A01=Christopher Damaren
A01=James R. Forbes
Age Group_Uncategorized
Age Group_Uncategorized
Author_Anton H. de Ruiter
Author_Christopher Damaren
Author_James R. Forbes
automatic-update
Category1=Non-Fiction
Category=TTDS
COP=United States
Delivery_Delivery within 10-20 working days
Language_English
PA=Available
Price_€50 to €100
PS=Active
softlaunch

Spacecraft Dynamics and Control: An Introduction

Provides the basics of spacecraft orbital dynamics plus attitude dynamics and control, using vectrix notation

Spacecraft Dynamics and Control: An Introduction presents the fundamentals of classical control in the context of spacecraft attitude control. This approach is particularly beneficial for the training of students in both of the subjects of classical control as well as its application to spacecraft attitude control. By using a physical system (a spacecraft) that the reader can visualize (rather than arbitrary transfer functions), it is easier to grasp the motivation for why topics in control theory are important, as well as the theory behind them.  The entire treatment of both orbital and attitude dynamics makes use of vectrix notation, which is a tool that allows the user to write down any vector equation of motion without consideration of a reference frame. This is particularly suited to the treatment of multiple reference frames. Vectrix notation also makes a very clear distinction between a physical vector and its coordinate representation in a reference frame. This is very important in spacecraft dynamics and control problems, where often multiple coordinate representations are used (in different reference frames) for the same physical vector.

  • Provides an accessible, practical aid for teaching and self-study with a layout enabling a fundamental understanding of the subject
  • Fills a gap in the existing literature by providing an analytical toolbox offering the reader a lasting, rigorous methodology for approaching vector mechanics, a key element vital to new graduates and practicing engineers alike
  • Delivers an outstanding resource for aerospace engineering students, and all those involved in the technical aspects of design and engineering in the space sector
  • Contains numerous illustrations to accompany the written text. Problems are included to apply and extend the material in each chapter

Essential reading for graduate level aerospace engineering students, aerospace professionals, researchers and engineers.

See more
Current price €88.34
Original price €92.99
Save 5%
A01=Anton H. de RuiterA01=Christopher DamarenA01=James R. ForbesAge Group_UncategorizedAuthor_Anton H. de RuiterAuthor_Christopher DamarenAuthor_James R. Forbesautomatic-updateCategory1=Non-FictionCategory=TTDSCOP=United StatesDelivery_Delivery within 10-20 working daysLanguage_EnglishPA=AvailablePrice_€50 to €100PS=Activesoftlaunch
Delivery/Collection within 10-20 working days
Product Details
  • Weight: 1202g
  • Dimensions: 170 x 249mm
  • Publication Date: 04 Jan 2013
  • Publisher: John Wiley & Sons Inc
  • Publication City/Country: United States
  • Language: English
  • ISBN13: 9781118342367

About Anton H. de RuiterChristopher DamarenJames R. Forbes

Anton de Ruiter Assistant Professor Mechanical and Aerospace Engineering Department Carleton University Ottawa Canada.Obtained his PhD in Aerospace Engineering from the University of Toronto in 2005.? Until 2006 he was a Visiting Research Fellow at the Space Technologies Branch of the Canadian Space Agency.?His interests include Nano-Satellite Technologies Interplanetary Missions Spacecraft Formation Flying Spacecraft Attitude and Orbit Determination and Control GPS-based Spacecraft Navigation Control Systems and Optimization Theory and Applications.?Professor De Ruiter has written extensively on spacecraft dynamics and related topics for journals articled papers and conference proceedings. Christopher J. Damaren Professor University of Toronto Institute for Aerospace Studies.Obtained his doctorate at UTIAS in 1990 in the area of control systems for flexible spacecraft. In the 1990's most of his research concentrated on control system design for large structurally flexible robot manipulator systems such as the Space Station robotic systems developed by Canada. Since joining the faculty of UTIAS in 1999 his research group has been involved in the dynamics and control of spacecraft including the orbital attitude and structural motions of these systems. James R. Forbes Assistant Professor Department of Mechanical Engineering McGill University.Obtained his doctorate at UTIAS in 2011 in the area of control system design with applications to aerospace systems including spacecraft attitude control. His teaching duties at McGill University include spacecraft dynamics and control courses at the upper undergraduate/beginning graduate level

Customer Reviews

Be the first to write a review
0%
(0)
0%
(0)
0%
(0)
0%
(0)
0%
(0)
We use cookies to ensure that we give you the best experience on our website. If you continue we'll assume that you are understand this. Learn more
Accept