Skip to main content
  • Book
  • © 2017

Satellite Formation Flying

Relative Dynamics, Formation Design, Fuel Optimal Maneuvers and Formation Maintenance

  • Systematically describes the concepts and principles for satellite formation from relative dynamics, formation design, and formation maneuvers to formation keeping and attitude synchronization
  • Proposes passive and periodic formations, which offer practical solutions to long-term satellite formation flying
  • Presents practical control methods for formation maneuver that bear in mind engineering constraints, such as fuel consumption and actuator constraints
  • Includes supplementary material: sn.pub/extras

Buy it now

Buying options

eBook USD 119.00
Price excludes VAT (USA)
  • Available as EPUB and PDF
  • Read on any device
  • Instant download
  • Own it forever
Softcover Book USD 159.99
Price excludes VAT (USA)
  • Compact, lightweight edition
  • Dispatched in 3 to 5 business days
  • Free shipping worldwide - see info
Hardcover Book USD 159.99
Price excludes VAT (USA)
  • Durable hardcover edition
  • Dispatched in 3 to 5 business days
  • Free shipping worldwide - see info

Tax calculation will be finalised at checkout

Other ways to access

This is a preview of subscription content, log in via an institution to check for access.

Table of contents (8 chapters)

  1. Front Matter

    Pages i-x
  2. Introduction

    • Danwei Wang, Baolin Wu, Eng Kee Poh
    Pages 1-7
  3. Dynamic Models of Satellite Relative Motion Around an Oblate Earth

    • Danwei Wang, Baolin Wu, Eng Kee Poh
    Pages 9-41
  4. Passive and Periodic Satellite Formation Design Around an Oblate Earth

    • Danwei Wang, Baolin Wu, Eng Kee Poh
    Pages 43-72
  5. Nonlinear Optimization of Low-Thrust Trajectory for Satellite Formation

    • Danwei Wang, Baolin Wu, Eng Kee Poh
    Pages 73-100
  6. Optimal Control for Satellite Formation Keeping

    • Danwei Wang, Baolin Wu, Eng Kee Poh
    Pages 101-130
  7. Conclusions

    • Danwei Wang, Baolin Wu, Eng Kee Poh
    Pages 193-196
  8. Back Matter

    Pages 197-205

About this book

This book systematically describes the concepts and principles for multi-satellite relative motion, passive and near passive formation designs, trajectory planning and control for fuel optimal formation maneuvers, and formation flying maintenance control design. As such, it provides a sound foundation for researchers and engineers in this field to develop further theories and pursue their implementations.

Though satellite formation flying is widely considered to be a major advance in space technology, there are few systematic treatments of the topic in the literature. Addressing that gap, the book offers a valuable resource for academics, researchers, postgraduate students and practitioners in the field of satellite science and engineering.

Authors and Affiliations

  • School of Electrical and Electronic Engineering, Nanyang Technological University, Singapore, Singapore

    Danwei Wang, Eng Kee Poh

  • Research Center of Satellite Technology, Harbin Institute of Technology, Harbin, China

    Baolin Wu

About the authors

Dr. Danwei Wang obtained his MSc and PhD degrees from the University of Michigan, Ann Arbor, in 1985 and 1989 respectively. Currently, he is a full-time professor in the school of Electrical and Electronic Engineering, and director of the Centre for E-City in Nanyang Technological University. His research domains include dynamics and control with applications, such as satellite control and robotics. Up to now, he has published more than 350 journal and conference papers with over 2500 SCI citations as of Feb 2015. Dr Wang is a senior member of IEEE and has served as general chair, technical program chair and many positions in numerous international academic conferences. Recently, Dr Wang has successfully concluded a few funded research projects on satellite formation flying and attitude control. These research projects have systematically studied the related topics for satellite formation flying.

Dr. Baolin Wu received the B.E and the M.E degrees in Aerospace Engineering from the Harbin Institute of Technology, Harbin, China, in 2003 and 2005 respectively, and the Ph.D. degree on the topic of satellite formation control from Nanyang Technological University, Singapore, in 2011. From 2011 to 2013, he worked as a research engineer on satellite attitude determination and control system in ST Electronics (Satellite Systems) Pte Ltd, Singapore. Since 2014, He has been with Research Center of Satellite Technology, Haribn Institute of Technology, China, where he is currently an Associate Professor. He was recognized as an outstanding young scholar by Harbin Institute of Technology in 2014. His current research interests are in the area of satellite formation control, trajectory optimization and attitude control.

Dr. Poh Eng Kee rceived his M. Sc (Elec. Eng.: Systems) and PhD (Elec. Eng.: Systems) from the University of Michigan in 1990 and 1993 respectively. Dr. Poh is presently a distinguished member of technical staff (DMTS) cum Laboratory Head (Guidance, Navigation and Control) in DSO, responsible for advancing guidance, navigation and control technologies development for applications in flight vehicles and unmanned platforms. Dr Poh is also an adjunct associate professor with the School of Electrical and Electrical Engineering, Nanyang Technological University.

Bibliographic Information

Buy it now

Buying options

eBook USD 119.00
Price excludes VAT (USA)
  • Available as EPUB and PDF
  • Read on any device
  • Instant download
  • Own it forever
Softcover Book USD 159.99
Price excludes VAT (USA)
  • Compact, lightweight edition
  • Dispatched in 3 to 5 business days
  • Free shipping worldwide - see info
Hardcover Book USD 159.99
Price excludes VAT (USA)
  • Durable hardcover edition
  • Dispatched in 3 to 5 business days
  • Free shipping worldwide - see info

Tax calculation will be finalised at checkout

Other ways to access