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

Dynamics and Control of Lorentz-Augmented Spacecraft Relative Motion

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
Related Subjects
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
http://library.link/vocab/cover_art
https://contentcafe2.btol.com/ContentCafe/Jacket.aspx?Return=1&Type=S&Value=9789811026034&userID=ebsco-test&password=ebsco-test
Dimensions
unknown
http://library.link/vocab/discovery_link
{'f': 'http://opac.lib.rpi.edu/record=b4386402'}
Extent
1 online resource (155 pages)
Form of item
online
Isbn
9789811026034
Media category
computer
Media MARC source
rdamedia
Media type code
c
Sound
unknown sound
Specific material designation
remote

Library Locations

    • Folsom LibraryBorrow it
      110 8th St, Troy, NY, 12180, US
      42.729766 -73.682577
Processing Feedback ...