عنوان

Spacecraft modeling, attitude determination, and control :

(Number (ISBN

0429446586

(Number (ISBN

042982212X

(Number (ISBN

0429822138

(Number (ISBN

0429822146

(Number (ISBN

9780429446580

(Number (ISBN

9780429822124

(Number (ISBN

9780429822131

(Number (ISBN

9780429822148

Erroneous ISBN

1138331503

Erroneous ISBN

9781138331501

Title Proper

Spacecraft modeling, attitude determination, and control :

General Material Designation

[Book]

Other Title Information

quaternion-based approach /

First Statement of Responsibility

Yaguang Yang (US Nuclear Regulatory Commission, Office of Research, Rockville, Maryland, USA).

Place of Publication, Distribution, etc.

Boca Raton, FL :

Name of Publisher, Distributor, etc.

CRC Press,

Date of Publication, Distribution, etc.

2019.

Specific Material Designation and Extent of Item

1 online resource

Text of Note

"A science publishers book."

Text of Note

Includes bibliographical references and index.

Text of Note

Introduction -- Orbit dynamics and properties -- Rotational sequences and quaternion -- Spacecraft dynamics and modeling -- Space environment and disturbance torques -- Spacecraft attitude determination -- Astronomical vector measurements -- Spacecraft attitude estimation -- Spacecraft attitude control -- Spacecraft actuators -- Spacecraft control using magnetic torques -- Attitude maneuver and orbit-raising -- Attitude mpc control -- Spacecraft control using cmg -- Spacecraft rendezvous and docking.

0

Text of Note

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.

Title

Spacecraft modeling, attitude determination, and control.

International Standard Book Number

9781138331501

Quaternions.

Rotational motion (Rigid dynamics)

Space vehicles-- Attitude control systems.

Stability of space vehicles.

Vector analysis.

Quaternions.

Rotational motion (Rigid dynamics)

Space vehicles-- Attitude control systems.

Stability of space vehicles.

TECHNOLOGY & ENGINEERING-- Engineering (General)

TECHNOLOGY-- Engineering-- Mechanical.

TECHNOLOGY-- Industrial Design-- General.

Vector analysis.

TEC-- 009000

TEC-- 009070

TEC-- 016000

TQ

Number

Edition

Class number

Book number

Yang, Yaguang

Date of Transaction

20200822162049.0

Cataloguing Rules (Descriptive Conventions))

pn

Electronic name

[Book]

Y