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Author : Arthur L. Greensite
Publisher : Unknown
Page : 140 pages
File Size : 51,6 Mb
Release : 1967
Category : Electronic
ISBN : UIUC:30112106583955
Author : Chong Hun Kim
Publisher : Lulu.com
Page : 676 pages
File Size : 52,5 Mb
Release : 2007
Category : Technology & Engineering
ISBN : 9780615165110
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 : Harry L. Runyan,A. Gerald Rainey
Publisher : Unknown
Page : 22 pages
File Size : 54,9 Mb
Release : 1961
Category : Launch vehicles (Astronautics)
ISBN : UIUC:30112104457913
Author : J.R. Wertz
Publisher : Springer Science & Business Media
Page : 877 pages
File Size : 55,8 Mb
Release : 2012-12-06
Category : Technology & Engineering
ISBN : 9789400999077
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.
Author : Bong Wie
Publisher : AIAA
Page : 692 pages
File Size : 51,6 Mb
Release : 1998
Category : Mathematics
ISBN : 1563472619
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 : Anonim
Publisher : Unknown
Page : 768 pages
File Size : 51,7 Mb
Release : 1994
Category : Aeronautics
ISBN : MINN:30000005901347
Author : United States. National Aeronautics and Space Administration
Publisher : Unknown
Page : 60 pages
File Size : 40,5 Mb
Release : 1970
Category : Space vehicles
ISBN : NASA:31769000661051
Author : United States. National Aeronautics and Space Administration Scientific and Technical Information Division
Publisher : Unknown
Page : 448 pages
File Size : 46,7 Mb
Release : 1968
Category : Aeronautics
ISBN : STANFORD:36105024714912
Author : Liang Yan,Haibin Duan,Yimin Deng
Publisher : Springer Nature
Page : 7455 pages
File Size : 45,9 Mb
Release : 2023-02-10
Category : Technology & Engineering
ISBN : 9789811966132
This book features the latest theoretical results and techniques in the field of guidance, navigation, and control (GNC) of vehicles and aircrafts. It covers a wide range of topics, including but not limited to, intelligent computing communication and control; new methods of navigation, estimation and tracking; control of multiple moving objects; manned and autonomous unmanned systems; guidance, navigation and control of miniature aircraft; and sensor systems for guidance, navigation and control etc. Presenting recent advances in the form of illustrations, tables, and text, it also provides detailed information of a number of the studies, to offer readers insights for their own research. In addition, the book addresses fundamental concepts and studies in the development of GNC, making it a valuable resource for both beginners and researchers wanting to further their understanding of guidance, navigation, and control.
Author : F. Landis Markley,John L. Crassidis
Publisher : Springer
Page : 486 pages
File Size : 42,6 Mb
Release : 2014-05-31
Category : Technology & Engineering
ISBN : 9781493908028
This book explores topics that are central to the field of spacecraft attitude determination and control. The authors provide rigorous theoretical derivations of significant algorithms accompanied by a generous amount of qualitative discussions of the subject matter. The book documents the development of the important concepts and methods in a manner accessible to practicing engineers, graduate-level engineering students and applied mathematicians. It includes detailed examples from actual mission designs to help ease the transition from theory to practice and also provides prototype algorithms that are readily available on the author’s website. Subject matter includes both theoretical derivations and practical implementation of spacecraft attitude determination and control systems. It provides detailed derivations for attitude kinematics and dynamics and provides detailed description of the most widely used attitude parameterization, the quaternion. This title also provides a thorough treatise of attitude dynamics including Jacobian elliptical functions. It is the first known book to provide detailed derivations and explanations of state attitude determination and gives readers real-world examples from actual working spacecraft missions. The subject matter is chosen to fill the void of existing textbooks and treatises, especially in state and dynamics attitude determination. MATLAB code of all examples will be provided through an external website.
Author : Anonim
Publisher : Unknown
Page : 1352 pages
File Size : 42,5 Mb
Release : 1967
Category : Government publications
ISBN : MINN:31951000578221G
Author : Anil K. Maini,Varsha Agrawal
Publisher : John Wiley & Sons
Page : 620 pages
File Size : 52,8 Mb
Release : 2011-06-09
Category : Science
ISBN : 9781119957270
A comprehensive, single-source reference on satellite technology and its applications, Satellite Technology: Principles and Applications, Second Editionincludes the latest developments on the topic. Covering the features and facilities of satellites and satellite launch vehicles, with an emphasis on the fundamental principles and concepts, the authors provide readers with a complete understanding of the technology. This book explains the past, present and future satellite missions, as well as non-communication related applications. Coverage ranges from remote sensing and navigational uses to meteorological and military areas. This second edition contains an additional chapter on earth station design and gives extensive focus to space based weapon systems, satellite interference and future trends in satellite technology. Extra information has also been provided on all of the first edition’s topics to enhance the existing coverage. Fully updated new edition with latest technological developments Covers the full range of important applications such remote sensing, weather forecasting, navigational, scientific and military applications Amply illustrated with figures and photographs, this book also contains problems with solutions, which is of benefit students at undergraduate and graduate levels An indispensible book for professionals and students in the field of satellite technology Companion website provides a complete and updated compendium on satellites and satellite launch vehicles
Author : Frederick A. Leve,Brian J. Hamilton,Mason A. Peck
Publisher : Springer
Page : 247 pages
File Size : 45,9 Mb
Release : 2015-10-17
Category : Technology & Engineering
ISBN : 9783319225630
The goal of this book is to serve both as a practical technical reference and a resource for gaining a fuller understanding of the state of the art of spacecraft momentum control systems, specifically looking at control moment gyroscopes (CMGs). As a result, the subject matter includes theory, technology, and systems engineering. The authors combine material on system-level architecture of spacecraft that feature momentum-control systems with material about the momentum-control hardware and software. This also encompasses material on the theoretical and algorithmic approaches to the control of space vehicles with CMGs. In essence, CMGs are the attitude-control actuators that make contemporary highly agile spacecraft possible. The rise of commercial Earth imaging, the advances in privately built spacecraft (including small satellites), and the growing popularity of the subject matter in academic circles over the past decade argues that now is the time for an in-depth treatment of the topic. CMGs are augmented by reaction wheels and related algorithms for steering all such actuators, which together comprise the field of spacecraft momentum control systems. The material is presented at a level suitable for practicing engineers and those with an undergraduate degree in mechanical, electrical, and/or aerospace engineering.
Author : Marcel J. Sidi
Publisher : Cambridge University Press
Page : 434 pages
File Size : 55,8 Mb
Release : 1997
Category : Science
ISBN : 0521787807
This 1997 book explains basic theory of spacecraft dynamics and control and the practical aspects of controlling a satellite.
Author : General Dynamics Corporation. Convair Division
Publisher : Unknown
Page : 128 pages
File Size : 42,6 Mb
Release : 1967
Category : Space vehicles
ISBN : OCLC:16726576