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Onboard Target Searching Strategy During Lost in Space Situations in Angles-Only Navigation Active Space Debris Removal

  • Yue YouEmail author
  • Hua Wang
Original Paper
  • 26 Downloads

Abstract

During the transition from ground-based to on-board relative navigation, active space debris removal faces the so-called lost in space problem where the target’s orbital parameters are known to a limited degree making its detection and identification among the other visible objects challenging. Being non-cooperative, the target is also assumed to be non-responsive to communication methods. Seven target search strategies are developed and evaluated using Monte-Carlo analysis. It is shown that one of the proposed methods, stepping-sweeping, can insure detection of the target within several minutes with a 99.9% success rate using either a single optical/infra-red camera payload. A sensitivity analysis was conducted on both the camera parameters and the detection success condition and reveals that this target search strategy is robust against initial position uncertainties. It is also applicable to all the common relative trajectories for orbital proximity operations. The developed tool can also be used for sensor parameters as well as search strategy key parameters selection.

Keywords

Onboard target searching Lost in space Angles-only navigation Linear covariance analysis Active debris removal 

Notes

Acknowledgements

The authors acknowledge financial support from the China Scholarship Council (number 201, 403, 160, 417), Space Engineering Center of École Polytechnique Fédérale de Lausanne, and the National Natural Science Foundation of China (number 11572345 and 11222215). The authors would like to thank the editor and the anonymous reviewers for their constructive comments.

References

  1. 1.
    Wormnes K, Le Letty R, Summerer L, Schonenborg R, Dubois-Matra O, Luraschi E et al (2013) ESA technologies for space debris remediation. In: Proceedings of the 6th IAASS conference: safety is not an option, Apr. 2013, pp 3–4Google Scholar
  2. 2.
    Esmiller B, Jacquelard C, Eckel HA, Wnuk E (2014) Space debris removal by ground-based lasers: main conclusions of the European project CLEANSPACE. Appl Opt 53(31):145–154CrossRefGoogle Scholar
  3. 3.
    Lee SC, Kim HD, Suk J (2012) Collision avoidance maneuver planning using GA for LEO and GEO satellite maintained in keeping area. Int J Aeronaut Space Sci 13(4):474–483CrossRefGoogle Scholar
  4. 4.
    Pelton JN (2015) Current space debris remediation and on-orbit servicing initiatives. New solutions for the space debris problem. Springer International Publishing, Cham, pp 11–29Google Scholar
  5. 5.
    Geller D (2007) Analysis of the relative attitude estimation and control problem for satellite inspection and orbital rendezvous. J Aeronaut Sci 55(2):195–214MathSciNetGoogle Scholar
  6. 6.
    Woffinden DC, Geller DK (2009) Optimal orbital rendezvous maneuvering for angles-only navigation. J Guidance Control Dyn 32(4):1382–1387CrossRefGoogle Scholar
  7. 7.
    Woffinden DC, Geller DK (2009) Observability criteria for angles-only navigation. Aerosp Electron Syst IEEE Trans 45(3):1194–1208CrossRefGoogle Scholar
  8. 8.
    Li JR, Li HY, Tang GJ, Luo YZ (2011) Research on the strategy of angles-only relative navigation for autonomous rendezvous. Sci China Technol Sci 54(7):1865–1872CrossRefzbMATHGoogle Scholar
  9. 9.
    Tombasco J, Axelrad P (2012) Along-track separation uncertainty modeling given space-based optical observations. J Guidance Control Dyn 35(3):732–739CrossRefGoogle Scholar
  10. 10.
    D’Amico S, Ardaens JS, Gaias G, Benninghoff H, Schlepp B, Jørgensen JL (2013) Noncooperative rendezvous using angles-only optical navigation: system design and flight results. J Guidance Control Dyn 36(6):1576–1595CrossRefGoogle Scholar
  11. 11.
    Grzymisch J, Fichter W (2014) Observability criteria and unobservable maneuvers for in-orbit bearings-only navigation. J Guidance Control Dyn 37(4):1250–1259CrossRefGoogle Scholar
  12. 12.
    LeGrand KA, DeMars KJ, Pernicka HJ (2015) Bearings-only initial relative orbit determination. J Guidance Control Dyn 38(9):1699–1713CrossRefGoogle Scholar
  13. 13.
    Geller DK, Perez A (2015) Initial relative orbit determination for close-in proximity operations. J Guidance Control Dyn 38(9):1833–1841CrossRefGoogle Scholar
  14. 14.
    Klein I, Geller DK (2015) Zero delta-V solution to the angles-only range observability problem during orbital proximity operations. In: Choukroun D, Oshman Y, Thienel J, Idan M (eds) Advances in estimation, navigation, and spacecraft control. Springer, Berlin, pp 351–369Google Scholar
  15. 15.
    Woffinden DC (2008) Angles-only navigation for autonomous orbital rendezvous. ProQuest, 2008Google Scholar
  16. 16.
    Schmidt J, Lovell TA (2008) Estimating geometric aspects of relative satellite motion using angles-only measurements. In: Proceedings of AIAA/AAS astrodynamics specialist conference and exhibit, Honolulu, Hawaii, 2008Google Scholar
  17. 17.
    Allen AC, Langley C, Mukherji R, Taylor AB, Umasuthan M, Barfoot TD (2008) Rendezvous lidar sensor system for terminal rendezvous, capture, and berthing to the international space station. In: SPIE defense and security symposium, international society for optics and photonics, 2008Google Scholar
  18. 18.
    Zimpfer D, Kachmar P, Tuohy S (2005) Autonomous rendezvous, capture and in-space assembly: past, present and future. In: 1st Space exploration conference: continuing the voyage of discovery, Orlando, Florida, USA, vol 1, Jan. 2005, pp 234–245Google Scholar
  19. 19.
    Rumford TE (2003) Demonstration of autonomous rendezvous technology (DART) project summary. In: AeroSense 2003, international society for optics and photonics, 2003Google Scholar
  20. 20.
    Weismuller T, Leinz M (2006) GN&C technology demonstrated by the orbital express autonomous rendezvous and capture sensor system. In: 29th Annual AAS guidance and control conference, Feb. 2006, pp 06–016Google Scholar
  21. 21.
    Carpenter JR (2011) A summary of the rendezvous, proximity operations, docking, and undocking (RPODU) lessons learned from the defense advanced research project agency (DARPA) orbital express (OE) demonstration system mission. NASA TM-2011-217088, 2011Google Scholar
  22. 22.
    Bodin P, Noteborn R, Larsson R, Karlsson T, D’Amico S, Ardaens JS, Berges JC (2012) The prisma formation flying demonstrator: overview and conclusions from the nominal mission. Adv Astronaut Sci 144:441–460Google Scholar
  23. 23.
    Noteborn R, Bodin P, Larsson R, Chasset C (2011) Flight results from the PRISMA optical line of sight based autonomous rendezvous experiment. In: 4th International conference on spacecraft formation flying missions and technologies, St-Hubert, Canada, 2011Google Scholar
  24. 24.
    Delpech M, Berges J-C, Karlsson T, Malbet F (2013) Results of PRISMA/FFIORD extended mission and applicability to future formation flying and active debris removal missions. Int J Space Sci Eng 1(4):382–409CrossRefGoogle Scholar
  25. 25.
    Thevenet JB (2008) A generic radio-frequency subsystem for high altitude formation flying missions. In: Proceedings of the 3rd international symposium on formation flying missions and technologies, Noordwijk, The Netherlands, 2008Google Scholar
  26. 26.
    Jørgensen JL, Denver T, Jørgensen PS (2004) Using an autonomous star tracker as formation flying sensor. Small Satell Syst Serv 571:1–5Google Scholar
  27. 27.
    Wanqing X, Liying T, Jing M, Yang L (2011) Received power attenuation analysis based on wavelet for reflection-style optical antenna deformations in free-space laser communications. Int J Antennas Propag.  https://doi.org/10.1155/2011/614536 Google Scholar
  28. 28.
    Zhou YP, Fu S, Yu SY et al (2010) Acquisition-probability model of nocooperative maneuvering target detection in space. Infrared Laser Eng 39(4):639–643Google Scholar
  29. 29.
    Jono T, Toyoda M, Nakagawa K et al (1999) Acquisition, tracking and pointing system of OICETS for flee space laser communications. SPIE 3692:4l–50Google Scholar
  30. 30.
    Bismoot A, Zaltzman A, Arnon S (2001) Novel method for acquisition and identification of satellites in a cluster for laser communication application. SPIE 4489:215–221Google Scholar
  31. 31.
    Feng GZ, Yang HJ, Qiu Q et al (2010) Analyzing from simulation of optimizing the spiral scan in the laser radar system. Infrared Laser Eng 35(2):165–168Google Scholar
  32. 32.
    Yu SY, Gao HD, Ma J et al (2002) Selection of acquisition scan methods in intersatellites optical communications. Chin J Lasers B 11(5):364–368Google Scholar
  33. 33.
    Stefan JF (2014) Lost in space. Master dissertation, Space Engineering Center, École Polytechnique Fédérale de Lausanne, Lausanne, Switzerland, 2014Google Scholar
  34. 34.
    You Y, Wang H, Paccolat C et al (2017) Time and covariance threshold triggered optimal uncooperative rendezvous using angles-only navigation. Int J Aerosp Eng 5451908:1–10CrossRefGoogle Scholar
  35. 35.
    You Y, Wang H, Tang GJ et al (2016) Simulation toolkit for onboard optimal maneuver planning in active debris removal using angles-only navigation. In: 2016 3rd International conference on information and communication technology for education (ICTE 2016), ISBN: 978-1-60595-372-4, Toronto, Canada, Aug. 02–03, 2016Google Scholar
  36. 36.
    You Y, Wang H, Paccolat C et al (2016) Square root unscented Kalman filter-based angles-only relative navigation using camera offset. J Astronaut 37(11):1312–1322 (in Chinese) Google Scholar
  37. 37.
    You Y, Wang H, Paccolat C et al (2017) Closed-loop covariance analysis for orbital rendezvous using square root UKF based angles-only navigation. J Natl Univ Def Technol 39(4):33–39 (in Chinese) Google Scholar
  38. 38.
    Fehse W (2003) Automated rendezvous and docking of spacecraft. Cambridge Univ Press, Cambridge, pp 424–440CrossRefGoogle Scholar
  39. 39.
    Geller DK (2006) Linear covariance techniques for orbital rendezvous analysis and autonomous onboard mission planning. J Guidance Control Dyn 29(6):1404–1414MathSciNetCrossRefGoogle Scholar
  40. 40.
    Li JR, Li HY, Tang GJ (2011) Optimal multi-objective trajectory design based on close-looped control for autonomous rendezvous. Sci China Technol Sci 54(11):3091–3097CrossRefGoogle Scholar
  41. 41.
    de Mijolla L, Cavrois B, Profizi A, Renault C, Cropp A (2013) Covariance analysis tool for far non-cooperative rendezvous. In: AIAA Guidance, Navigation, and Control Conference, AIAA, Boston, MA, 2013, pp 1–16Google Scholar

Copyright information

© The Korean Society for Aeronautical & Space Sciences 2019

Authors and Affiliations

  1. 1.Naval Research AcademyBeijingPeople’s Republic of China
  2. 2.College of Aerospace Science and EngineeringNational University of Defense TechnologyChangshaPeople’s Republic of China

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