Dynamics and Control of Lorentz-Augmented Spacecraft Relative Motion

Transcription

1 Dynamics and Control of Lorentz-Augmented Spacecraft Relative Motion

2 Ye Yan Xu Huang Yueneng Yang Dynamics and Control of Lorentz-Augmented Spacecraft Relative Motion 123

3 Ye Yan College of Aerospace Science and Engineering National University of Defense Technology Changsha, Hunan China Yueneng Yang College of Aerospace Science and Engineering National University of Defense Technology Changsha, Hunan China Xu Huang College of Aerospace Science and Engineering National University of Defense Technology Changsha, Hunan China ISBN ISBN (ebook) DOI / Library of Congress Control Number: Springer Science+Business Media Singapore 2017 This work is subject to copyright. All rights are reserved by the Publisher, whether the whole or part of the material is concerned, specifically the rights of translation, reprinting, reuse of illustrations, recitation, broadcasting, reproduction on microfilms or in any other physical way, and transmission or information storage and retrieval, electronic adaptation, computer software, or by similar or dissimilar methodology now known or hereafter developed. The use of general descriptive names, registered names, trademarks, service marks, etc. in this publication does not imply, even in the absence of a specific statement, that such names are exempt from the relevant protective laws and regulations and therefore free for general use. The publisher, the authors and the editors are safe to assume that the advice and information in this book are believed to be true and accurate at the date of publication. Neither the publisher nor the authors or the editors give a warranty, express or implied, with respect to the material contained herein or for any errors or omissions that may have been made. Printed on acid-free paper This Springer imprint is published by Springer Nature The registered company is Springer Nature Singapore Pte Ltd. The registered company address is: 152 Beach Road, #22-06/08 Gateway East, Singapore , Singapore

4 To my wife, Q. Huang, and my daughter, J. Yan Ye Yan To my parents, G. Huang and X. Ling, for their love Xu Huang To my parents, Z. Yang and A. Lin, my wife, J. Sun, and my daughter, Z. Yang Yueneng Yang

5 Preface Lorentz spacecraft is a new conceptional space vehicle. It actively generates electrostatic charge on its surface to induce Lorentz force via interaction with the ambient planetary magnetic field. The induced Lorentz force could be used as propellantless magnetic propulsion for orbital maneuvering. Traditional spacecraft rely on the thrusters to perform such maneuvers, and the maneuvering capability is strongly restricted by the amount of the available propellant onboard. Differently, the conception of Lorentz spacecraft provides a propellantless means to solve this problem, thus greatly enhancing the maneuvering capability and extending the mission duration. Due to this compelling advantage in saving fuels, dynamics and control of this new vehicle have raised great research interests. This book aims to investigate the dynamics and control of Lorentz-augmented spacecraft relative motion. It consists of three parts, including introduction, theoretical analysis, and applications. The first part (Chap. 1) gives a detailed review on the theoretical and experimental developments of Lorentz spacecraft. Also, this chapter introduces three types of typical space missions. That is, spacecraft hovering, formation flying, and rendezvous, which all belong to the category of relative orbital motion. The second part (Chap. 2) develops theoretical models of Lorentzaugmented spacecraft relative motion about arbitrary elliptic orbits in both two-body and J 2 -perturbed environment. Also, these models explicitly include the magnetic dipole tilt angle, which are more representative of the Earth s magnetic field, and are expected to derive more precise results. The third part (Chap. 3, 4, 5 and 6) proposes detailed relative navigation and control strategies for Lorentz-augmented space missions. Two navigation schemes for Lorentz spacecraft relative motion are introduced and compared in Chap. 3. The remaining three chapters elaborate the control schemes for Lorentz-augmented spacecraft hovering, formation flying, and rendezvous, respectively. Both optimal open-loop and closed-loop controllers are designed for these typical applications. We have conducted the related research works since I wish to acknowledge my Ph.D. Student, Xu Huang, for his concentrated devotion in this study. His creative thinking and persistent diligence impress me very much. I particularly appreciate his contributions to the fulfillment of this book. Also, special thanks to all vii

6 viii Preface the scientists and researchers who preceded us in the theoretical and experimental developments of Lorentz spacecraft. Furthermore, this work was supported in part by the Fund of Innovation of the Graduate School of the National University of Defense Technology under Grant B140106, and in part by the by the Hunan Provincial Innovation Foundation for Postgraduate under Grant CX2014B006. Changsha, Hunan, China Ye Yan

7 Contents 1 Introduction Background Review Lorentz Spacecraft Spacecraft Relative Motion Outline of the Book... 6 References Dynamical Model of Lorentz-Augmented Orbital Motion Model of Absolute Orbital Motion Geomagnetic Field Two-Body Model J 2 -Perturbed Model Model of Relative Orbital Motion Two-Body Model Analytical Solutions to Two-Body Model J 2 -Perturbed Model Conclusions References Relative Navigation of Lorentz-Augmented Orbital Motion State and Observation Equations State Equation of Relative Translational Motion State Equation of Relative Rotational Motion Observation Equation Filtering Algorithm for Relative Navigation EKF Algorithm UKF Algorithm Numerical Simulations Conclusions References ix

8 x Contents 4 Dynamics and Control of Lorentz-Augmented Spacecraft Hovering Problem Formulation and Dynamical Model Problem Formulation Dynamical Model Case of Two-Body Circular Reference Orbit Open-Loop Control Closed-Loop Control Numerical Simulation Case of Two-Body Elliptic Reference Orbit Open-Loop Control Closed-Loop Control Numerical Simulation Case of J 2 -Perturbed Reference Orbit Dynamical Model Open-Loop Control Numerical Simulation Conclusions References Dynamics and Control of Lorentz-Augmented Spacecraft Formation Flying Problem Formulation and Dynamical Model Problem Formulation Dynamical Model Case of Two-Body Circular Reference Orbit Formation Configurations in Circular Orbits Problem Formulation Open-Loop Control Closed-Loop Control Numerical Simulation Case of Two-Body Elliptic Reference Orbit Formation Configurations in Elliptic Orbits Open-Loop Control Closed-Loop Control Numerical Simulation Conclusions References Dynamics and Control of Lorentz-Augmented Spacecraft Rendezvous Problem Formulation and Dynamical Model Problem Formulation Dynamical Model

9 Contents xi 6.2 Case of Two-Body Reference Orbit Open-Loop Control Closed-Loop Control Numerical Simulation Case of J 2 -Perturbed Reference Orbit Dynamical Model Open-Loop Control Numerical Simulations Conclusions References Appendix