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The Resource Dynamics and Control of Lorentz-Augmented Spacecraft Relative Motion

Dynamics and Control of Lorentz-Augmented Spacecraft Relative Motion

Creator
Contributor
Language
eng
Work
Publication
Extent
1 online resource (155 pages)
Contents
  • Preface -- Contents -- 1 Introduction -- 1.1 Background -- 1.2 Review -- 1.2.1 Lorentz Spacecraft -- 1.2.2 Spacecraft Relative Motion -- 1.3 Outline of the Book -- References -- 2 Dynamical Model of Lorentz-Augmented Orbital Motion -- 2.1 Model of Absolute Orbital Motion -- 2.1.1 Geomagnetic Field -- 2.1.2 Two-Body Model -- 2.1.3 J2-Perturbed Model -- 2.2 Model of Relative Orbital Motion -- 2.2.1 Two-Body Model -- 2.2.1.1 Equations of Relative Motion -- 2.2.1.2 The Lorentz Force -- 2.2.2 Analytical Solutions to Two-Body Model -- 2.2.2.1 Approximate Analytical Solutions -- 2.2.2.2 Numerical Simulations -- 2.2.3 J2-Perturbed Model -- 2.2.3.1 Equations of J2-Perturbed Relative Motion -- 2.2.3.2 Numerical Simulations -- 2.3 Conclusions -- References -- 3 Relative Navigation of Lorentz-Augmented Orbital Motion -- 3.1 State and Observation Equations -- 3.1.1 State Equation of Relative Translational Motion -- 3.1.2 State Equation of Relative Rotational Motion -- 3.1.3 Observation Equation -- 3.2 Filtering Algorithm for Relative Navigation -- 3.2.1 EKF Algorithm -- 3.2.2 UKF Algorithm -- 3.2.3 Numerical Simulations -- 3.3 Conclusions -- References -- 4 Dynamics and Control of Lorentz-Augmented Spacecraft Hovering -- 4.1 Problem Formulation and Dynamical Model -- 4.1.1 Problem Formulation -- 4.1.2 Dynamical Model -- 4.1.2.1 Equations of Relative Motion -- 4.1.2.2 The Lorentz Acceleration -- 4.2 Case of Two-Body Circular Reference Orbit -- 4.2.1 Open-Loop Control -- 4.2.1.1 Equatorial Circular Orbit with Nontilted Dipole -- 4.2.1.2 Inclined Circular Orbit with Nontilted Dipole -- 4.2.1.3 Inclined Circular Orbit with Tilted Dipole -- 4.2.2 Closed-Loop Control -- 4.2.3 Numerical Simulation -- 4.2.3.1 Equatorial Circular Orbit with Nontilted Dipole -- 4.2.3.2 Inclined Circular Orbit with Nontilted Dipole -- 4.2.3.3 Inclined Circular Orbit with Tilted Dipole
  • 4.3 Case of Two-Body Elliptic Reference Orbit -- 4.3.1 Open-Loop Control -- 4.3.2 Closed-Loop Control -- 4.3.3 Numerical Simulation -- 4.3.3.1 Open-Loop Control -- 4.3.3.2 Closed-Loop Control -- 4.4 Case of J2-Perturbed Reference Orbit -- 4.4.1 Dynamical Model -- 4.4.2 Open-Loop Control -- 4.4.3 Numerical Simulation -- 4.5 Conclusions -- References -- 5 Dynamics and Control of Lorentz-Augmented Spacecraft Formation Flying -- 5.1 Problem Formulation and Dynamical Model -- 5.1.1 Problem Formulation -- 5.1.2 Dynamical Model -- 5.2 Case of Two-Body Circular Reference Orbit -- 5.2.1 Formation Configurations in Circular Orbits -- 5.2.1.1 PCO Configuration -- 5.2.1.2 GCO Configuration -- 5.2.2 Problem Formulation -- 5.2.2.1 Initial Condition Constraints -- 5.2.2.2 Final Condition Constraints -- 5.2.2.3 Path Constraints -- 5.2.3 Open-Loop Control -- 5.2.4 Closed-Loop Control -- 5.2.5 Numerical Simulation -- 5.2.5.1 Formation Establishment -- 5.2.5.2 Formation Reconfiguration -- 5.2.5.3 Effect of the Dipole Tilt Angle -- 5.3 Case of Two-Body Elliptic Reference Orbit -- 5.3.1 Formation Configurations in Elliptic Orbits -- 5.3.2 Open-Loop Control -- 5.3.3 Closed-Loop Control -- 5.3.4 Numerical Simulation -- 5.3.4.1 Open-Loop Controller -- 5.3.4.2 Closed-Loop Controller -- 5.4 Conclusions -- References -- 6 Dynamics and Control of Lorentz-Augmented Spacecraft Rendezvous -- 6.1 Problem Formulation and Dynamical Model -- 6.1.1 Problem Formulation -- 6.1.2 Dynamical Model -- 6.2 Case of Two-Body Reference Orbit -- 6.2.1 Open-Loop Control -- 6.2.2 Closed-Loop Control -- 6.2.3 Numerical Simulation -- 6.2.3.1 Case with Fixed Final Time -- 6.2.3.2 Case with Free Final Time -- 6.3 Case of J2-Perturbed Reference Orbit -- 6.3.1 Dynamical Model -- 6.3.2 Open-Loop Control -- 6.3.3 Numerical Simulations -- 6.4 Conclusions -- References -- Appendix
Isbn
9789811026034
Link
http://libproxy.rpi.edu/login?url=https://ebookcentral.proquest.com/lib/rpi/detail.action?docID=4728165
Instance
Label
Dynamics and Control of Lorentz-Augmented Spacecraft Relative Motion
Title
Dynamics and Control of Lorentz-Augmented Spacecraft Relative Motion
Creator
Contributor
Subject
Language
eng
Cataloging source
MiAaPQ
Literary form
non fiction
Nature of contents
dictionaries
Dynamics and Control of Lorentz-Augmented Spacecraft Relative Motion
Label
Dynamics and Control of Lorentz-Augmented Spacecraft Relative Motion
Link
http://libproxy.rpi.edu/login?url=https://ebookcentral.proquest.com/lib/rpi/detail.action?docID=4728165
Publication
Copyright
Related Contributor
Related Location
Related Agents
Related Authorities
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Carrier category
online resource
Carrier category code
cr
Carrier MARC source
rdacarrier
Color
multicolored
Content category
text
Content type code
txt
Content type MARC source
rdacontent
Contents
  • Preface -- Contents -- 1 Introduction -- 1.1 Background -- 1.2 Review -- 1.2.1 Lorentz Spacecraft -- 1.2.2 Spacecraft Relative Motion -- 1.3 Outline of the Book -- References -- 2 Dynamical Model of Lorentz-Augmented Orbital Motion -- 2.1 Model of Absolute Orbital Motion -- 2.1.1 Geomagnetic Field -- 2.1.2 Two-Body Model -- 2.1.3 J2-Perturbed Model -- 2.2 Model of Relative Orbital Motion -- 2.2.1 Two-Body Model -- 2.2.1.1 Equations of Relative Motion -- 2.2.1.2 The Lorentz Force -- 2.2.2 Analytical Solutions to Two-Body Model -- 2.2.2.1 Approximate Analytical Solutions -- 2.2.2.2 Numerical Simulations -- 2.2.3 J2-Perturbed Model -- 2.2.3.1 Equations of J2-Perturbed Relative Motion -- 2.2.3.2 Numerical Simulations -- 2.3 Conclusions -- References -- 3 Relative Navigation of Lorentz-Augmented Orbital Motion -- 3.1 State and Observation Equations -- 3.1.1 State Equation of Relative Translational Motion -- 3.1.2 State Equation of Relative Rotational Motion -- 3.1.3 Observation Equation -- 3.2 Filtering Algorithm for Relative Navigation -- 3.2.1 EKF Algorithm -- 3.2.2 UKF Algorithm -- 3.2.3 Numerical Simulations -- 3.3 Conclusions -- References -- 4 Dynamics and Control of Lorentz-Augmented Spacecraft Hovering -- 4.1 Problem Formulation and Dynamical Model -- 4.1.1 Problem Formulation -- 4.1.2 Dynamical Model -- 4.1.2.1 Equations of Relative Motion -- 4.1.2.2 The Lorentz Acceleration -- 4.2 Case of Two-Body Circular Reference Orbit -- 4.2.1 Open-Loop Control -- 4.2.1.1 Equatorial Circular Orbit with Nontilted Dipole -- 4.2.1.2 Inclined Circular Orbit with Nontilted Dipole -- 4.2.1.3 Inclined Circular Orbit with Tilted Dipole -- 4.2.2 Closed-Loop Control -- 4.2.3 Numerical Simulation -- 4.2.3.1 Equatorial Circular Orbit with Nontilted Dipole -- 4.2.3.2 Inclined Circular Orbit with Nontilted Dipole -- 4.2.3.3 Inclined Circular Orbit with Tilted Dipole
  • 4.3 Case of Two-Body Elliptic Reference Orbit -- 4.3.1 Open-Loop Control -- 4.3.2 Closed-Loop Control -- 4.3.3 Numerical Simulation -- 4.3.3.1 Open-Loop Control -- 4.3.3.2 Closed-Loop Control -- 4.4 Case of J2-Perturbed Reference Orbit -- 4.4.1 Dynamical Model -- 4.4.2 Open-Loop Control -- 4.4.3 Numerical Simulation -- 4.5 Conclusions -- References -- 5 Dynamics and Control of Lorentz-Augmented Spacecraft Formation Flying -- 5.1 Problem Formulation and Dynamical Model -- 5.1.1 Problem Formulation -- 5.1.2 Dynamical Model -- 5.2 Case of Two-Body Circular Reference Orbit -- 5.2.1 Formation Configurations in Circular Orbits -- 5.2.1.1 PCO Configuration -- 5.2.1.2 GCO Configuration -- 5.2.2 Problem Formulation -- 5.2.2.1 Initial Condition Constraints -- 5.2.2.2 Final Condition Constraints -- 5.2.2.3 Path Constraints -- 5.2.3 Open-Loop Control -- 5.2.4 Closed-Loop Control -- 5.2.5 Numerical Simulation -- 5.2.5.1 Formation Establishment -- 5.2.5.2 Formation Reconfiguration -- 5.2.5.3 Effect of the Dipole Tilt Angle -- 5.3 Case of Two-Body Elliptic Reference Orbit -- 5.3.1 Formation Configurations in Elliptic Orbits -- 5.3.2 Open-Loop Control -- 5.3.3 Closed-Loop Control -- 5.3.4 Numerical Simulation -- 5.3.4.1 Open-Loop Controller -- 5.3.4.2 Closed-Loop Controller -- 5.4 Conclusions -- References -- 6 Dynamics and Control of Lorentz-Augmented Spacecraft Rendezvous -- 6.1 Problem Formulation and Dynamical Model -- 6.1.1 Problem Formulation -- 6.1.2 Dynamical Model -- 6.2 Case of Two-Body Reference Orbit -- 6.2.1 Open-Loop Control -- 6.2.2 Closed-Loop Control -- 6.2.3 Numerical Simulation -- 6.2.3.1 Case with Fixed Final Time -- 6.2.3.2 Case with Free Final Time -- 6.3 Case of J2-Perturbed Reference Orbit -- 6.3.1 Dynamical Model -- 6.3.2 Open-Loop Control -- 6.3.3 Numerical Simulations -- 6.4 Conclusions -- References -- Appendix
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Extent
1 online resource (155 pages)
Form of item
online
Isbn
9789811026034
Media category
computer
Media MARC source
rdamedia
Media type code
c
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