عنوان

Spacecraft modeling, attitude determination, and control :

شابک

0429446586

شابک

042982212X

شابک

0429822138

شابک

0429822146

شابک

9780429446580

شابک

9780429822124

شابک

9780429822131

شابک

9780429822148

شابک اشتباه

1138331503

شابک اشتباه

9781138331501

عنوان اصلي

Spacecraft modeling, attitude determination, and control :

نام عام مواد

[Book]

ساير اطلاعات عنواني

quaternion-based approach /

نام نخستين پديدآور

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

محل نشرو پخش و غیره

Boca Raton, FL :

نام ناشر، پخش کننده و غيره

CRC Press,

تاریخ نشرو بخش و غیره

2019.

نام خاص و کميت اثر

1 online resource

متن يادداشت

"A science publishers book."

متن يادداشت

Includes bibliographical references and index.

متن يادداشت

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.

بدون عنوان

0

متن يادداشت

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.

عنوان

Spacecraft modeling, attitude determination, and control.

شماره استاندارد بين المللي کتاب و موسيقي

9781138331501

موضوع مستند نشده

Quaternions.

موضوع مستند نشده

Rotational motion (Rigid dynamics)

موضوع مستند نشده

Space vehicles-- Attitude control systems.

موضوع مستند نشده

Stability of space vehicles.

موضوع مستند نشده

Vector analysis.

موضوع مستند نشده

Quaternions.

موضوع مستند نشده

Rotational motion (Rigid dynamics)

موضوع مستند نشده

Space vehicles-- Attitude control systems.

موضوع مستند نشده

Stability of space vehicles.

موضوع مستند نشده

TECHNOLOGY & ENGINEERING-- Engineering (General)

موضوع مستند نشده

TECHNOLOGY-- Engineering-- Mechanical.

موضوع مستند نشده

TECHNOLOGY-- Industrial Design-- General.

موضوع مستند نشده

Vector analysis.

موضوع مستند نشده

TEC-- 009000

موضوع مستند نشده

TEC-- 009070

موضوع مستند نشده

TEC-- 016000

موضوع مستند نشده

TQ

شماره

ويراست

شماره رده

نشانه اثر

مستند نام اشخاص تاييد نشده

Yang, Yaguang

تاريخ عمليات

20200822162049.0

قواعد فهرست نويسي ( بخش توصيفي )

pn

نام الکترونيکي

نوع ماده

[Book]

تكميل شده

Y