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Author: Dong Ye Publisher: Academic Press ISBN: 0323954561 Category : Technology & Engineering Languages : en Pages : 280
Book Description
Fast Satellite Attitude Maneuver and Control introduces the concept of agile satellites and corresponding fast maneuver attitude control systems, systematically and comprehensively presenting recent research results of fast maneuver attitude control for agile satellites by using advanced nonlinear control techniques. This reference book focuses on modeling and attitude control, considering different actuator combinations, actuator installation deviation, actuator fault, and flexible appendage coupling effect for agile satellites. The book provides a unified platform for understanding and applicability of agile satellites fast maneuverer and stabilization control for different purposes. It will be an excellent resource for researchers working on spacecraft design, nonlinear control systems, vehicle systems and complex control systems. Unifies existing and emerging concepts concerning nonlinear control theory, fault tolerant, and attitude control for agile satellites Provides a series of the latest results, including, but not limited to, fast maneuverer and stabilization control, hybrid actuator control, nonlinear attitude control, fault tolerant control, and active vibration suppression towards agile satellites Comprehensively captures recent advances of theory, technological aspects and applications of fast maneuverer and stabilization control in agile satellites Addresses research problems in each chapter, along with numerical and simulation results that reflect engineering practice and demonstrate the focus of developed analysis and synthesis approaches Contains comprehensive, up-to-date references, which play an indicative role for further study
Author: Dong Ye Publisher: Academic Press ISBN: 0323954561 Category : Technology & Engineering Languages : en Pages : 280
Book Description
Fast Satellite Attitude Maneuver and Control introduces the concept of agile satellites and corresponding fast maneuver attitude control systems, systematically and comprehensively presenting recent research results of fast maneuver attitude control for agile satellites by using advanced nonlinear control techniques. This reference book focuses on modeling and attitude control, considering different actuator combinations, actuator installation deviation, actuator fault, and flexible appendage coupling effect for agile satellites. The book provides a unified platform for understanding and applicability of agile satellites fast maneuverer and stabilization control for different purposes. It will be an excellent resource for researchers working on spacecraft design, nonlinear control systems, vehicle systems and complex control systems. Unifies existing and emerging concepts concerning nonlinear control theory, fault tolerant, and attitude control for agile satellites Provides a series of the latest results, including, but not limited to, fast maneuverer and stabilization control, hybrid actuator control, nonlinear attitude control, fault tolerant control, and active vibration suppression towards agile satellites Comprehensively captures recent advances of theory, technological aspects and applications of fast maneuverer and stabilization control in agile satellites Addresses research problems in each chapter, along with numerical and simulation results that reflect engineering practice and demonstrate the focus of developed analysis and synthesis approaches Contains comprehensive, up-to-date references, which play an indicative role for further study
Author: Naval Postgraduate Naval Postgraduate School Publisher: ISBN: Category : Languages : en Pages : 169
Book Description
Time-optimal spacecraft rotations have been developed and implemented on orbiting spacecraft, highlighting opportunities for improving slew performance. Double-digit reductions in the time required to slew from one attitude to another have been demonstrated. However, the ability to perform mission planning to make use of minimum time slewing maneuvers is largely precluded by the need to compute a numerical solution to find a single minimum time maneuver control trajectory. Machine learning approaches can eliminate the need to generate problem solutions by approximating time-optimal maneuver times with sufficient accuracy for planning using only the initial and final attitude requirements. The advantages of time-optimal spacecraft maneuvers, a planning construct for evaluating legacy and machine learning maneuver time generators, and the machine learning processes that enable this approach are outlined. Compared to legacy planning techniques, time-optimal slew approximations yield target collection increases of 3% to 24% for an example planning framework.
Author: Publisher: ISBN: Category : Aeronautics Languages : en Pages : 652
Book Description
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
Author: Dirk H. De Does Publisher: ISBN: Category : Space vehicles Languages : en Pages : 0
Book Description
This report considers the problem of controlling both the attitude and angular velocities of an axially symmetric spacecraft while minimizing the maneuver duration. In particular, various combinations of thrust limited reaction jets are employed to properly orient a spinning space body with respect to specified reference directions starting from known initial conditions of the vehicle's attitude and angular rates. Five control jet configurations are considered: two gimballed systems where torques can be applied about, (1) any axis in a plane normal to the axis of symmetry, (2) two perpendicular non- rotating axis in a plane normal to the axis of symmetry; and three body-fixed configurations where the thrusters are immobile relative to the vehicle and can provide both positive and negative or only positive (negative) control torques about one or both of the vehicle's transverse axis. The control systems are realizable from a hardware standpoint and the corresponding optimal controls can be classified as: (1) a continuous function of time, (2) bang-bang, (3) on-off, and (4) a combination of (1 and 2) or (2 and 3).
Author: J.R. Wertz Publisher: Springer Science & Business Media ISBN: 9400999070 Category : Technology & Engineering Languages : en Pages : 877
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.
Author: Jason Hall Publisher: BoD – Books on Demand ISBN: 9533075511 Category : Technology & Engineering Languages : en Pages : 612
Book Description
The development and launch of the first artificial satellite Sputnik more than five decades ago propelled both the scientific and engineering communities to new heights as they worked together to develop novel solutions to the challenges of spacecraft system design. This symbiotic relationship has brought significant technological advances that have enabled the design of systems that can withstand the rigors of space while providing valuable space-based services. With its 26 chapters divided into three sections, this book brings together critical contributions from renowned international researchers to provide an outstanding survey of recent advances in spacecraft technologies. The first section includes nine chapters that focus on innovative hardware technologies while the next section is comprised of seven chapters that center on cutting-edge state estimation techniques. The final section contains eleven chapters that present a series of novel control methods for spacecraft orbit and attitude control.
Author: Dong Ye
Author: Dong Ye
Author: Naval Postgraduate Naval Postgraduate School
Author: Stuart C. Brown
Author: Alan W. Hewston
Author: 
Author: 
Author: Dirk H. De Does
Author: J.R. Wertz
Author: Jason Hall
Author: John D. Regetz (Jr.)