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Record Nr. |
UNINA9910627243503321 |
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Autore |
Fichter Walter |
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Titolo |
Principles of spacecraft control : concepts and theory for practical applications / / Walter Fichter, Ramin T. Geshnizjani |
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Pubbl/distr/stampa |
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Cham, Switzerland : , : Springer, , [2023] |
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©2023 |
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ISBN |
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Descrizione fisica |
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1 online resource (202 pages) |
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Disciplina |
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Soggetti |
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Space vehicles - Control systems |
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Lingua di pubblicazione |
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Formato |
Materiale a stampa |
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Livello bibliografico |
Monografia |
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Nota di bibliografia |
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Includes bibliographical references and index. |
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Nota di contenuto |
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Intro -- Preface -- Contents -- Acronyms -- List of Symbols -- 1 System Engineering Basics -- 1.1 Objectives and Interfaces of Control Systems -- 1.2 Functional Architecture and Environment -- 1.2.1 Overview and Terminology -- 1.2.2 External Disturbances -- 1.2.3 Sensors -- 1.2.4 Actuators -- 1.3 Design Process -- 1.4 System Design Rules -- 1.4.1 Performance -- 1.4.2 Actuator Sizing -- 1.4.3 Processing and Software -- 1.4.4 Redundancy -- 1.5 Budgets and Specifications -- 1.5.1 Key Parameters -- 1.5.2 Specific Performance Parameters -- References -- 2 Satellite Motion Models -- 2.1 Rotational Kinematics -- 2.1.1 Attitude Parametrization -- 2.1.2 Conversions -- 2.1.3 Differential Equations -- 2.1.4 Two-Axis Inertial Pointing -- 2.2 Single-Body Spacecraft and Gyrostat -- 2.2.1 Dynamics of Rotation and Translation -- 2.2.2 Wheel Dynamics -- 2.2.3 Gravitational Force and Torque -- 2.2.4 Multiple Wheels and Summary -- 2.3 Single-Body Spacecraft with Control Moment Gyros -- 2.3.1 Rotational Dynamics -- 2.3.2 Flywheel and Gimbal Dynamics -- 2.3.3 Summary and CMG Array Dynamics -- 2.3.4 Singularities -- 2.4 Multi-Body Spacecraft with Test Mass -- 2.4.1 Equations of Motion -- 2.4.2 Discussion -- References -- 3 Rotational State Determination -- 3.1 Attitude Determination -- 3.1.1 Concepts and the Two Unit Vector Case -- 3.1.2 Three or More Unit Vector Measurements -- 3.2 Angular Rate Estimation -- 3.3 Attitude Observation and Filtering -- 3.3.1 Concept of a Kinematic Model -- 3.3.2 Yaw Observation During Earth Pointing |
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