Author: Anna D. Guerman
Publisher:
ISBN:
Category : Astrodynamics
Languages : en
Pages : 1728
Book Description
First IAA Conference on Dynamics and Control of Space Systems 2012
Author: Anna D. Guerman
Publisher:
ISBN:
Category : Astrodynamics
Languages : en
Pages : 1728
Book Description
Publisher:
ISBN:
Category : Astrodynamics
Languages : en
Pages : 1728
Book Description
Dynamics and Control of Space Systems DyCoSS2012
Second IAA Conference on Dynamics and Control of Space Systems 2014
Author: IAA Conference on Dynamics and Control of Space Systems
Publisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
Second IAA Conference on Dynamics and Control of Space Systems 2014
Author:
Publisher:
ISBN: 9780877036180
Category : Astrodynamics
Languages : en
Pages : 0
Book Description
Publisher:
ISBN: 9780877036180
Category : Astrodynamics
Languages : en
Pages : 0
Book Description
Fourth IAA Conference on Dynamics and Control of Space Systems 2018
Author: Ya-Zhong Luo
Publisher:
ISBN:
Category : Astrodynamics
Languages : en
Pages : 2414
Book Description
Publisher:
ISBN:
Category : Astrodynamics
Languages : en
Pages : 2414
Book Description
Spacecraft Modeling, Attitude Determination, and Control
Author: Yaguang Yang
Publisher: CRC Press
ISBN: 0429822146
Category : Science
Languages : en
Pages : 328
Book Description
This book discusses all spacecraft attitude control-related topics: spacecraft (including attitude measurements, actuator, and disturbance torques), modeling, spacecraft attitude determination and estimation, and spacecraft attitude controls. Unlike other books addressing these topics, this book focuses on quaternion-based methods because of its many merits. The book lays a brief, but necessary background on rotation sequence representations and frequently used reference frames that form the foundation of spacecraft attitude description. It then discusses the fundamentals of attitude determination using vector measurements, various efficient (including very recently developed) attitude determination algorithms, and the instruments and methods of popular vector measurements. With available attitude measurements, attitude control designs for inertial point and nadir pointing are presented in terms of required torques which are independent of actuators in use. Given the required control torques, some actuators are not able to generate the accurate control torques, therefore, spacecraft attitude control design methods with achievable torques for these actuators (for example, magnetic torque bars and control moment gyros) are provided. Some rigorous controllability results are provided. The book also includes attitude control in some special maneuvers, such as orbital-raising, docking and rendezvous, that are normally not discussed in similar books. Almost all design methods are based on state-spaced modern control approaches, such as linear quadratic optimal control, robust pole assignment control, model predictive control, and gain scheduling control. Applications of these methods to spacecraft attitude control problems are provided. Appendices are provided for readers who are not familiar with these topics.
Publisher: CRC Press
ISBN: 0429822146
Category : Science
Languages : en
Pages : 328
Book Description
This book discusses all spacecraft attitude control-related topics: spacecraft (including attitude measurements, actuator, and disturbance torques), modeling, spacecraft attitude determination and estimation, and spacecraft attitude controls. Unlike other books addressing these topics, this book focuses on quaternion-based methods because of its many merits. The book lays a brief, but necessary background on rotation sequence representations and frequently used reference frames that form the foundation of spacecraft attitude description. It then discusses the fundamentals of attitude determination using vector measurements, various efficient (including very recently developed) attitude determination algorithms, and the instruments and methods of popular vector measurements. With available attitude measurements, attitude control designs for inertial point and nadir pointing are presented in terms of required torques which are independent of actuators in use. Given the required control torques, some actuators are not able to generate the accurate control torques, therefore, spacecraft attitude control design methods with achievable torques for these actuators (for example, magnetic torque bars and control moment gyros) are provided. Some rigorous controllability results are provided. The book also includes attitude control in some special maneuvers, such as orbital-raising, docking and rendezvous, that are normally not discussed in similar books. Almost all design methods are based on state-spaced modern control approaches, such as linear quadratic optimal control, robust pole assignment control, model predictive control, and gain scheduling control. Applications of these methods to spacecraft attitude control problems are provided. Appendices are provided for readers who are not familiar with these topics.
Second IAA Conference on Dynamics and Control of Space Systems 2014: Space structures and tethers
Author: Filippo Graziani
Publisher:
ISBN:
Category : Astrodynamics
Languages : en
Pages : 1781
Book Description
Publisher:
ISBN:
Category : Astrodynamics
Languages : en
Pages : 1781
Book Description
Second IAA Conference on Dynamics and Control of Space Systems 2014: Satellite constellations and formation flying I
Author: Filippo Graziani
Publisher:
ISBN:
Category : Astrodynamics
Languages : en
Pages : 1781
Book Description
Publisher:
ISBN:
Category : Astrodynamics
Languages : en
Pages : 1781
Book Description
Third IAA Conference on Dynamics and Control of Space Systems 2017
Author: Yury N. Razoumny
Publisher:
ISBN: 9780877036432
Category : Astrodynamics
Languages : en
Pages : 1200
Book Description
Publisher:
ISBN: 9780877036432
Category : Astrodynamics
Languages : en
Pages : 1200
Book Description