Attitude Control During Launch PDF Download
Are you looking for read ebook online? Search for your book and save it on your Kindle device, PC, phones or tablets. Download Attitude Control During Launch PDF full book. Access full book title Attitude Control During Launch by Arthur L. Greensite. Download full books in PDF and EPUB format.
Author: Arthur L. Greensite
Publisher:
ISBN:
Category :
Languages : en
Pages : 140
Get Book Here
Book Description
Author: Arthur L. Greensite
Publisher:
ISBN:
Category :
Languages : en
Pages : 140
Get Book Here
Book Description
Author: Arthur L. Greensite
Publisher:
ISBN:
Category : Space vehicles
Languages : en
Pages : 126
Get Book Here
Book Description
Author: Chong Hun Kim
Publisher: Lulu.com
ISBN: 0615165117
Category : Technology & Engineering
Languages : en
Pages : 676
Get Book Here
Book Description
This book is written for aerospace engineers who have completed their BS degree and are interested in the design and analysis of rocket attitude control systems. It introduces a new approach to the design, characterized by its robustness. Current LV attitude control systems are designed based on classical SISO control theory, and they lack robustness. The theory used here truly offers a technique that enables us to design control systems that are reasonably insensitive to math modeling errors and can withstand disturbances such as gust, and in addition it doesn’t need external states estimator, such as Kalman filtering. Extensive simulation results, which demonstrate the effectiveness of this approach, are presented in this book. Basic rocket theory and a concept of H-infinity control system design technique are explained for those who are new in these fields of study.
Author: A.L. Greensite
Publisher:
ISBN:
Category :
Languages : en
Pages :
Get Book Here
Book Description
Author: General Dynamics Corporation. Convair Division
Publisher:
ISBN:
Category : Space vehicles
Languages : en
Pages :
Get Book Here
Book Description
Author: Bong Wie
Publisher: AIAA
ISBN: 9781563472619
Category : Mathematics
Languages : en
Pages : 692
Get Book Here
Book Description
A textbook that incorporates the latest methods used for the analysis of spacecraft orbital, attitude, and structural dynamics and control. Spacecraft dynamics is treated as a dynamic system with emphasis on practical applications, typical examples of which are the analysis and redesign of the pointing control system of the Hubble Space Telescope and the analysis of an active vibrations control for the COFS (Control of Flexible Structures) Mast Flight System. In addition to the three subjects mentioned above, dynamic systems modeling, analysis, and control are also discussed. Annotation copyrighted by Book News, Inc., Portland, OR
Author: Harry L. Runyan
Publisher:
ISBN:
Category : Launch vehicles (Astronautics)
Languages : en
Pages : 22
Get Book Here
Book Description
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 140
Get Book Here
Book Description
Author: A. L. Greensite
Publisher:
ISBN:
Category :
Languages : en
Pages :
Get Book Here
Book Description
Author: J.R. Wertz
Publisher: Springer Science & Business Media
ISBN: 9400999070
Category : Technology & Engineering
Languages : en
Pages : 877
Get Book Here
Book Description
Roger D. Werking Head, Attitude Determination and Control Section National Aeronautics and Space Administration/ Goddard Space Flight Center Extensiye work has been done for many years in the areas of attitude determination, attitude prediction, and attitude control. During this time, it has been difficult to obtain reference material that provided a comprehensive overview of attitude support activities. This lack of reference material has made it difficult for those not intimately involved in attitude functions to become acquainted with the ideas and activities which are essential to understanding the various aspects of spacecraft attitude support. As a result, I felt the need for a document which could be used by a variety of persons to obtain an understanding of the work which has been done in support of spacecraft attitude objectives. It is believed that this book, prepared by the Computer Sciences Corporation under the able direction of Dr. James Wertz, provides this type of reference. This book can serve as a reference for individuals involved in mission planning, attitude determination, and attitude dynamics; an introductory textbook for stu dents and professionals starting in this field; an information source for experimen ters or others involved in spacecraft-related work who need information on spacecraft orientation and how it is determined, but who have neither the time nor the resources to pursue the varied literature on this subject; and a tool for encouraging those who could expand this discipline to do so, because much remains to be done to satisfy future needs.
