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Navigation and Guidance of Orbital Transfer Vehicle

  • Xuefeng Li
  • Chaobing Li

Part of the Navigation: Science and Technology book series (NASTECH)

Table of contents

  1. Front Matter
    Pages i-xiv
  2. Xuefeng Li, Chaobing Li
    Pages 1-4
  3. Xuefeng Li, Chaobing Li
    Pages 13-26
  4. Xuefeng Li, Chaobing Li
    Pages 27-41
  5. Xuefeng Li, Chaobing Li
    Pages 43-72
  6. Xuefeng Li, Chaobing Li
    Pages 73-87
  7. Xuefeng Li, Chaobing Li
    Pages 121-161
  8. Xuefeng Li, Chaobing Li
    Pages 163-174
  9. Xuefeng Li, Chaobing Li
    Pages E1-E1

About this book

Introduction

This book uses the entire flying process, starting from ground launching of the orbital transfer vehicle (OTV) to injecting payload into earth synchronous orbit, as an example for real-world engineering practices. It discusses in detail the analysis design and integrated OTV navigation and guidance system technologies in combination with the engineering experiences of the authors in analysis, design and integrated OTV navigation and guidance system applications, and the research on navigation and guidance theories. It focuses on establishing motion of air vehicle equations, control system hardware components, orbit prediction technology, inertial navigation and initial alignment technologies, INS/GNSS integrated navigation technologies, INS/CNS integrated navigation technologies, redundant fault tolerance and failure reconfiguration technology of inertial sensors, guidance and midcourse correction technologies and orbit control strategies.

The book is a valuable reference book for the engineers, technicians and researchers who are engaged in analysis, design and integrated application of OTV navigation and guidance control systems. It can also be used as teaching material for postgraduates and senior undergraduates majoring in OTV navigation and guidance systems and other related subjects.

Keywords

Orbital Transfer Vehicle system OTV launch Space navigation Control system Orbit prediction Motional equation Inertial navigation Initial alignment Navigation technology Orbit control Orbital Transfer Vehicle

Authors and affiliations

  • Xuefeng Li
    • 1
  • Chaobing Li
    • 2
  1. 1.Beijing Aerospace Automatic Control InstituteBeijingChina
  2. 2.Beijing Aerospace Automatic Control InstituteBeijingChina

Bibliographic information

  • DOI https://doi.org/10.1007/978-981-10-6334-3
  • Copyright Information Springer Nature Singapore Pte Ltd. and National Defense Industry Press, Beijing 2018
  • Publisher Name Springer, Singapore
  • eBook Packages Engineering
  • Print ISBN 978-981-10-6333-6
  • Online ISBN 978-981-10-6334-3
  • Series Print ISSN 2522-0454
  • Series Online ISSN 2522-0462
  • Buy this book on publisher's site