Produktbild: Orbital Mechanics & Formation

Orbital Mechanics & Formation A Digital Control Perspective

Fr. 272.00

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Beschreibung

Produktdetails

Einband

Gebundene Ausgabe

Erscheinungsdatum

01.10.2011

Verlag

Elsevier Science & Technology

Seitenzahl

438

Maße (L/B/H)

23.4/15.6/2.5 cm

Gewicht

1100 g

Sprache

Englisch

ISBN

978-0-85709-054-6

Beschreibung

Produktdetails

Einband

Gebundene Ausgabe

Erscheinungsdatum

01.10.2011

Verlag

Elsevier Science & Technology

Seitenzahl

438

Maße (L/B/H)

23.4/15.6/2.5 cm

Gewicht

1100 g

Sprache

Englisch

ISBN

978-0-85709-054-6

EU-Ansprechpartner

Zeitfracht Medien GmbH
Ferdinand-Jühlke-Straße 7
99095 Erfurt
DE
produktsicherheit@zeitfracht.de

Herstelleradresse

Elsevier Science & Technology
125 London Wall
EC2Y 5AS London
GB
tradeorders@elsevier.com

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  • Produktbild: Orbital Mechanics & Formation
  • Dedication

    List of figures

    List of tables

    List of symbols

    Acknowledgements

    Preface

    About the authors

    Chapter 1: Introduction

    1.1 Introduction to the book

    1.2 Book division

    Chapter 2: Two body orbital motion

    Abstract:

    2.1 Introduction to orbital motion

    2.2 Constraints and generalized coordinates

    2.3 Lagrange's equation

    2.4 System of particles

    2.5 Two body orbital motion problem

    2.6 Orbital equations of motion

    2.7 Energy and velocity of orbiting bodies

    2.8 Escape velocity

    2.9 Earth Coordinate Inertial (ECI) system

    2.10 Period of an orbit

    2.11 Development of Kepler's equation

    2.12 Suggested problems

    Chapter 3: Orbital perturbations in the two body motion

    Abstract:

    3.1 Introduction to disturbance effects

    3.2 Lagrange planetary equations

    3.3 Perturbation due to the earth oblateness

    3.4 The near-Earth atmosphere effects

    3.5 Solar radiation pressure force

    3.6 Other disturbance effects

    3.7 Suggested problems

    Chapter 4: Frame rotations and quaternions

    Abstract:

    4.1 Introduction to rotations and quaternions

    4.2 Two-dimensional frame rotations

    4.3 Three-dimensional frame rotations

    4.4 Example of frame rotations

    4.5 Quaternion definition and rotations

    4.6 Quaternion to Euler angle relations

    4.7 Suggested problems

    Chapter 5: Rigid body motion

    Abstract:

    5.1 Introduction to attitude dynamics

    5.2 Rate of change of a vector

    5.3 Moment of inertia

    5.4 Principal moments of inertia

    5.5 Energy formulation

    5.6 Rate of change of a quaternion

    5.7 Ares V equations of motion

    5.8 Suggested problems

    Chapter 6: Environmental and actuator torques

    Abstract:

    6.1 Introduction to torque formulation

    6.2 Environmental torques

    6.3 Actuator (or control) torques

    6.4 Suggested problems

    Chapter 7: Continuous and digital control systems

    Abstract:

    7.1 Introduction to methods of designing continuous and discrete control systems

    7.2 Ares V equations of motion for first stage flight

    7.3 Continuous control formulation

    7.4 Discrete control formulation

    7.5 Adaptive and intelligent controls

    7.6 Suggested problems

    Chapter 8: Example

    Abstract:

    8.1 Introduction to examples in spacecraft attitude dynamics and control

    8.2 Nanosatellite problem definition

    8.3 B-dot controller for fast corrections

    8.4 Linear quadratic regulator for attitude correction

    8.5 Linear quadratic regulator control weight design

    8.6 Suggested problems

    Chapter 9: Formation flying

    Abstract:

    9.1 Introduction to formation flying

    9.2 Tschauner-Hempel formulation

    9.3 Clohessy-Wiltshire formulation

    9.4 Earth oblateness and solar effects in formation flying

    9.5 Lawden solution

    9.6 Discrete optimal control problem for formation flying

    9.7 Formation flying controller implementation

    9.8 Suggested problems

    Chapter 10: Deployment procedure for a constellation

    Abstract:

    10.1 Introductory comments

    10.2 Desired conditions of the satellites in the proposed tetrahedron constellation

    10.3 Transfer from a circular orbit to the elliptical orbit (stage 1)

    10.4 Station-keeping procedure (stage 2)

    10.5 Deployment procedure for the tetrahedron constellation

    10.6 Remarks

    10.7 Suggested problems

    Chapter 11: Reconfiguration procedure for a constellation

    Abstract:

    11.1 Introduction to the reconfiguration process of a constellation

    11.2 Data mining process of the Lagrange planetary equations

    11.3 Fuzzy logic controller

    11.4 Phase I to II in-plane motion fuzzy log