Skip to main content
Log in

Survey of the electrostatic tractor research for reorbiting passive GEO space objects

  • Review Article
  • Published:
Astrodynamics Aims and scope Submit manuscript

A Correction to this article was published on 11 February 2022

This article has been updated

Abstract

The number of operational satellites and debris objects in the valuable geosynchronous ring has increased steadily over time such that active debris removal missions are necessary to ensure long-term stability. These objects are very large and tumbling, making any mission scenarios requiring physical contact very challenging. In the last 10 years, the concept of using an electrostatic tractor has been investigated extensively. With the electrostatic tractor concept, active charge emission is employed to simultaneously charge the tug or services vehicle, while aiming the charge exhaust onto the passive space debris object to charge it as well. The resulting electrostatic force has been explored to actuate this debris object to a disposal orbit or to detumble the object, all without physical contact. This paper provides a survey of the related research and reviews the charging concepts, the associated electrostatic force and torque modeling, and the feedback control developments, as well as the charge sensing research.

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

Access this article

Price excludes VAT (USA)
Tax calculation will be finalised during checkout.

Instant access to the full article PDF.

Similar content being viewed by others

Change history

References

  1. Schaub, H., Moorer, D. F. Jr. Geosynchronous large debris reorbiter: challenges and prospects. The Journal of the Astronautical Sciences, 2012, 59(1–2): 161–176.

    Article  Google Scholar 

  2. Schaub, H., Sternovsky, Z. Active space debris charging for contactless electrostatic disposal maneuvers. Advances in Space Research, 2014, 53(1): 110–118.

    Article  Google Scholar 

  3. Hogan, E. A., Schaub, H. Relative motion control for two-spacecraft electrostatic orbit corrections. Journal of Guidance, Control, and Dynamics, 2013, 36(1): 240–249.

    Article  Google Scholar 

  4. Lai, S. T. Fundamentals of spacecraft charging: spacecraft interactions with space plasmas. Princeton University Press, 2011.

    Google Scholar 

  5. Chen, F. F. Introduction to plasma physics and controlled fusion: volume 1: plasma physics, 2nd ed. Plenum Press, 1984.

    Google Scholar 

  6. Schaub, H., Sternovsky, Z. Active space debris charging for contactless electrostatic disposal maneuvers. The 6th European Conference on Space Debris, 2013.

    Google Scholar 

  7. Denton, M. H., Thomsen, M. F., Korth, H., Lynch, S., Zhang, J. C., Liemohn, M. W. Bulk plasma properties at geosynchronous orbit. Journal of Geophysical Research, 2005, 110(A7): A07223.

    Article  Google Scholar 

  8. Seubert, C. R., Stiles, L. A., Schaub, H. Effective coulomb force modeling for spacecraft in earth orbit plasmas. Advances in Space Research, 2014, 54(2): 209–220.

    Article  Google Scholar 

  9. Murdoch, N., Izzo, D., Bombardelli, C., Carnelli, I., Hilgers, A., Rodgers, D. Electrostatic tractor for near earth object de ection. The 59th International Astronautical Congress, 2008.

    Google Scholar 

  10. Murdoch, N., Izzo, D., Bombardelli, C., Carnelli, I., Hilgers, A., Rodgers, D. The electrostatic tractor for asteroid de ection. The 58th International Astronautical Congress, 2008.

    Google Scholar 

  11. Cover, J. H. Jr., Knauer, W., Maurer, H. A. Lightweight re ecting structures utilizing electrostatic in ation: USA, 3546706. 1970–12–08.

  12. King, L. B., Parker, G. G., Deshmukh, S., Chong, J. H. Spacecraft formation- ying using inter-vehicle coulomb forces. NASA Institute for Advanced Concepts, 2002.

    Google Scholar 

  13. Kong, E. M. C., Miller, D. W., Sedwick, R. J. Exploiting orbital dynamics for aperture synthesis using distributed satellite systems: applications to visible earth imager system. Proceedings of AAS/AIAA Space flight Mechanics Meeting, 1999.

    Google Scholar 

  14. King, L. B., Parker, G. G., Deshmukh, S., Chong, J. H. Study of interspacecraft coulomb forces and implications for formation flying. Journal of Propulsion and Power, 2003, 19(3): 497–505.

    Article  Google Scholar 

  15. Schaub, H., Parker, G. G., King, L. B. Challenges and prospect of coulomb formations. The Journal of the Astronautical Sciences, 2004, 52(1–2): 169–193.

    Article  MathSciNet  Google Scholar 

  16. Natarajan, A., Schaub, H. Linear dynamics and stability analysis of a two-craft coulomb tether formation. Journal of Guidance, Control, and Dynamics, 2006, 29(4): 831–839.

    Article  Google Scholar 

  17. Berryman, J., Schaub, H. Analytical charge analysis for two- and three-craft coulomb formations. Journal of Guidance, Control, and Dynamics, 2007, 30(6): 1701–1710.

    Article  Google Scholar 

  18. Schaub, H., Hall, C. D., Berryman, J. Necessary conditions for circularly-restricted static coulomb formations. The Journal of the Astronautical Sciences, 2006, 54(3–4): 525–541.

    Article  MathSciNet  Google Scholar 

  19. Vasavada, H., Schaub, H. Analytic solutions for equal mass four-craft static coulomb formation. The Journal of the Astronautical Sciences, 2008, 56(1): 17–40.

    Article  Google Scholar 

  20. Moorer, D. F., Schaub, H. Hybrid electrostatic space tug: USA, 8210480. 2012–07–03.

  21. Moorer, D. F., Schaub, H. Electrostatic spacecraft reorbiter: USA, WO/2011/019830. 2011–02–17.

  22. Bennett, T., Stevenson, D., Hogan, E., Schaub, H. Prospects and challenges of touchless electrostatic detumbling of small bodies. Advances in Space Research, 2015, 56(3): 557–568.

    Article  Google Scholar 

  23. Yasaka, T., Hanada, T., Hirayama, H. Geo debris environment: a model to forecast the next 100 years. Advances in Space Research, 1999, 23(1): 191–199.

    Article  Google Scholar 

  24. IADC. Proceedings of the 15th Inter-Agency Space Debris Coordination Committee Meeting, NASA JSC, Houston, TX, 1997.

    Google Scholar 

  25. Johnson, N. L. Protecting the GEO environment: policies and practices. Space Policy, 1999, 15(3): 127–135.

    Article  Google Scholar 

  26. Jehn, R., Agapov, V., Hernndez, C. The situation in the geostationary ring. Advances in Space Research, 2005, 35(7): 1318–1327.

    Article  Google Scholar 

  27. Schaub, H., Jasper, L. E. Z., Anderson, P. V., McKnight, D. S. Cost and risk assessment for spacecraft operation decisions caused by the space debris environment. Acta Astronautica, 2015, 113: 66–79.

    Article  Google Scholar 

  28. Oltrogge, D. L., Kelso, T. S. Getting to know our space population from the public catalog. AIAA/AAS Astrodynamics Specialist Conference, 2011.

    Google Scholar 

  29. Anderson, P. V., Schaub, H. Local orbital debris flux study in the geostationary ring. Advances in Space Research, 2013, 51(12): 2195–2206.

    Article  Google Scholar 

  30. Anderson, P. V., Schaub, H. Local debris congestion in the geosynchronous environment with population augmentation. Acta Astronautica, 2014, 94(2): 619–628.

    Article  Google Scholar 

  31. McKnight, D. S., Di Pentino, F. R. New insights on the orbital debris collision hazard at GEO. Acta Astronautica, 2013, 85: 73–82.

    Article  Google Scholar 

  32. McKnight, D. Pay me now or pay me more later: start the development of active orbital debris removal now. Advanced Maui Optical and Space Surveillance Technologies Conference, 2010.

    Google Scholar 

  33. Chrystal, P., McKnight, D., Meredith, P. L., Schmidt, J., Fok, M., Wetton, C. Space debris: on collision course for insurers? Swiss Reinsurance Company Ltd, 2011.

    Google Scholar 

  34. Oltrogge, D. L., Alfano, S., Law, C., Cacioni, A., Kelso, T. S. A comprehensive assessment of collision likelihood in geosynchronous earth orbit. The 68th International Astronautical Congress, 2017.

    Google Scholar 

  35. Carlson, E., Casali, S., Chambers, D., Geissler, G., Lalich, A., Leipold, M., Mach, R., Parry, J., Weems, F. Final design of a space debris removal system. NASA-CR-189976, NASA, 1990.

    Google Scholar 

  36. Reed, J., Barraclough, S. Development of harpoon system for capturing space debris. The 6th European Conference on Space Debris, 2013.

    Google Scholar 

  37. Dudziak, R., Tuttle, S., Barraclough, S. Harpoon technology development for the active removal of space debris. Advances in Space Research, 2015, 56(3): 509–527.

    Article  Google Scholar 

  38. Loughman, J. J. Overview and analysis of the soldier satellite concept for removal of space debris. AIAA Space 2010 Conference & Exposition, 2010.

    Google Scholar 

  39. Forshaw, J. L., Aglietti, G. S., Salmon, T., Retat, I., Roe, M., Burgess, C., Chabot, T., Pisseloup, A., Phipps, A., Bernal, C. et al. Final payload test results for the removedebris active debris removal mission. Acta Astronautica, 2017, 138: 326–342.

    Article  Google Scholar 

  40. Jasper, L. Z., Schaub, H. Input shaped large thrust maneuver with a tethered debris object. The 6th European Conference on Space Debris, 2013.

    Google Scholar 

  41. Jasper, L. E. Z., Seubert, C. R., Schaub, H., Trushkyakov, V., Yutkin, E. Tethered tug for large low earth orbit debris removal. AAS/AIAA Astrodynamics Specialists Conference, 2012.

    Google Scholar 

  42. Jasper, L., Schaub, H. Input shaped large thrust maneuver with a tethered debris object. Acta Astronautica, 2014, 96: 128–137.

    Article  Google Scholar 

  43. Nishida, S. I., Kawamoto, S., Okawa, Y., Terui, F., Kitamura, S. Space debris removal system using a small satellite. Acta Astronautica, 2009, 65(1–2): 95–102.

    Article  Google Scholar 

  44. Nishida, S. I., Kikuchi, N. A scenario and technologies for space debris removal. The 12th International Symposium on Artificial Intelligence, Robotics and Automation in Space, 2014.

    Google Scholar 

  45. Castronuovo, M. M. Active space debris removal a preliminary mission analysis and design. Acta Astronautica, 2011, 69(9–10): 848–859.

    Article  Google Scholar 

  46. Smith, D. A., Martin, C., Kassebom, M., Petersen, H., Shaw, A., Skidmore, B., Smith, D., Stokes, H., Willig, A. A mission to preserve the geostationary region. Advances in Space Research, 2004, 34(5): 1214–1218.

    Article  Google Scholar 

  47. Lennon, J. A., Henshaw, C. G., Purdy, W. An architecture for autonomous control of a robotic satellite grappling mission. AIAA Guidance, Navigation and Control Conference and Exhibit, 2008.

    Google Scholar 

  48. Couzin, P., Teti, F., Rembala, R. Active removal of large debris: rendez-vous and robotic capture issues. The 2nd European Workshop on Active Debris Removal, 2012.

    Google Scholar 

  49. Karavaev, Y. S., Kopyatkevich, R. M., Mishina, M. N., Mishin, G. S., Papushev, P. G., Shaburov, P. N. The dynamic properties of rotation and optical characteristics of space debris at geostationary orbit. Advances in the Astronautical Sciences, 2004, 119: 1457–1466.

    Google Scholar 

  50. DeLuca, L. T., Bernelli, F., Maggi, F., Tadini, P., Pardini, C., Anselmo, L., Grassi, M., Pavarin, D., Francesconi, A., Branz, F. et al. Active space debris removal by a hybrid propulsion module. Acta Astronautica, 2013, 91: 20–33.

    Article  Google Scholar 

  51. Schonenborg, R. A. C., Schoyer, H. F. R. Solid propulsion de-orbiting and re-orbiting. In: Proceedings of the 5th European Conference on Space Debris, 2009.

    Google Scholar 

  52. Vetrisano, M., Thiry, N., Vasile, M. Detumbling large space debris via laser ablation. 2015 IEEE Aerospace Conference, 2015.

    Google Scholar 

  53. Ortiz Gómez, N., Walker, S. J. I. Eddy currents applied to de-tumbling of space debris: analysis and validation of approximate proposed methods. Acta Astronautica, 2015, 114: 34–53.

    Article  Google Scholar 

  54. Bombardelli, C., Peláez, J. Ion beam shepherd for contactless space debris removal. Journal of Guidance, Control, and Dynamics, 2011, 34(3): 916–920.

    Article  Google Scholar 

  55. Bombardelli, C., Urrutxua, H., Merino, M., Ahedo, E., Peláez, J., Olympio, J. Dynamics of ion-beam-propelled space debris. The 22nd International Symposium on Space Flight Dynamics, 2011.

    Google Scholar 

  56. Merino, M., Ahedo Galilea, E., Bombardelli, C., Urrutxua, H., Pélaez Álvarez, J., Summerer, L. Space debris removal with an ion beam shepherd satellite: target-plasma interaction. The 47th AIAA/ASME/SAE/ ASEE Joint Propulsion Conference & Exhibit, 2011.

    Google Scholar 

  57. Schaub, H., Jasper, L. E. Z. Circular orbit radius control using electrostatic actuation for 2-craft configurations. AAS/AIAA Astrodynamics Specialists Conference, 2011.

    Google Scholar 

  58. Schaub, H., Stevenson, D. Prospects of relative attitude control using coulomb actuation. The Journal of the Astronautical Sciences, 2013, 60(3–4): 258–277.

    Article  Google Scholar 

  59. Garrett, H. B., Whittlesey, A. C. Guide to mitigating spacecraft charging effects. Wiley, 2012.

    Google Scholar 

  60. Lai, S. T. Spacecraft charging. American Institute of Aeronautics & Astronautics, 2011.

    Google Scholar 

  61. Whipple, E. C. Potentials of surfaces in space. Reports on Progress in Physics, 1981, 44(11): 1197–1250.

    Article  Google Scholar 

  62. Mullen, E. G., Gussenhoven, M. S., Hardy, D. A., Aggson, T. A., Ledley, B. G., Whipple, E. Scatha survey of high-level spacecraft charging in sunlight. Journal of Geophysical Research, 1986, 91(A2): 1474–1490.

    Article  Google Scholar 

  63. Lai, S. T., Tautz, M. F. Aspects of spacecraft charging in sunlight. IEEE Transactions on Plasma Science, 2006, 34(5): 2053–2061.

    Article  Google Scholar 

  64. Smythe, W. R. Static and dynamic electricity, 3rd ed. McGraw-Hill, 1968.

    MATH  Google Scholar 

  65. Stevenson, D., Schaub, H. Multi-sphere method for modeling spacecraft electrostatic forces and torques. Advances in Space Research, 2013, 51(1): 10–20.

    Article  Google Scholar 

  66. Peck, M. A. Prospects and challenges for lorentz- augmented orbits. AIAA Guidance, Navigation, and Control Conference and Exhibit, 2005.

    Google Scholar 

  67. Hogan, E. A., Schaub, H. Impacts of hot space plasma and ion beam emission on electrostatic tractor performance. IEEE Transactions on Plasma Science, 2015, 43(9): 3115–3129.

    Article  Google Scholar 

  68. Hogan, E. A., Schaub, H. Space weather in uence on relative motion control using the touchless electrostatic tractor. The Journal of the Astronautical Sciences, 2016, 63(3): 237–262.

    Article  Google Scholar 

  69. Hughes, J., Schaub, H. Prospects of using a pulsed electrostatic tractor with nominal geosynchronous conditions. IEEE Transactions on Plasma Science, 2017, 45(8): 1887–1897.

    Article  Google Scholar 

  70. Hughes, J., Schaub, H. Orbital and solar storm analysis of the pulsed electrostatic tractor. The 7th European Conference on Space Debris, 2017.

    Google Scholar 

  71. Stevenson, D. Optimization of sphere population for electrostatic multi sphere model. The 12th Spacecraft Charging Technology Conference, 2012.

    Google Scholar 

  72. Lekner, J. Electrostatics of two charged conducting spheres. Proceedings of the Royal Society A, 2012, 468: 2829–2848.

    Article  MathSciNet  MATH  Google Scholar 

  73. Gibson, W. C. The method of moments in electromagnetics. Chapman & Hall, 2007.

    Google Scholar 

  74. Ingram, G., Hughes, J., Bennett, T., Reily, C., Schaub, H. Autonomous volume multi-sphere-model development using electric field matching. AAS Space ight Mechanics Meeting, 2017.

    Google Scholar 

  75. Chow, P., Hughes, J., Bennett, T., Schaub, H. Automated sphere geometry optimization for the volume multi-sphere method. AAS/AIAA Space ight Mechanics Meeting, 2016.

    Google Scholar 

  76. Stevenson, D., Schaub, H. Optimization of sphere population for electrostatic multi-sphere method. IEEE Transactions on Plasma Science, 2013, 41(12): 3526–3535.

    Article  Google Scholar 

  77. Maxwell, J. C. A treatise on electricity and magnetism. Clarendon Press, 1873.

    Google Scholar 

  78. Jackson, J. D. Classical electrodynamics. John Wiley & Sons, 1999.

    Google Scholar 

  79. Price, S. L., Stone, A. J., Alderton, M. Explicit formulae for the electrostatic energy, forces and torques between a pair of molecules of arbitrary symmetry. Molecular Physics, 1984, 52(4): 987–1001.

    Article  Google Scholar 

  80. Hou, X. Y., Scheeres, D. J., Xin, X. S. Mutual potential between two rigid bodies with arbitrary shapes and mass distributions. Celestial Mechanics and Dynamical Astronomy, 2017, 127(3): 369–395.

    Article  MathSciNet  MATH  Google Scholar 

  81. Hughes, J., Schaub, H. Spacecraft electrostatic force and torque expansions yielding appropriate fidelity measures. AAS Space ight Mechanics Meeting, 2017.

    Google Scholar 

  82. Berryman, J., Schaub, H. Static equilibrium configurations in GEO coulomb spacecraft formations. The 15th AAS/AIAA Space Flight Mechanics Meeting, 2005.

    Google Scholar 

  83. Schaub, H. Stabilization of satellite motion relative to a coulomb spacecraft formation. Journal of Guidance, Control, and Dynamics, 2005, 28(6): 1231–1239.

    Article  Google Scholar 

  84. Wang, S. Q., Schaub, H. Spacecraft collision avoidance using coulomb forces with separation distance and rate feedback. Journal of Guidance, Control, and Dynamics, 2008, 31(3): 740–750.

    Article  Google Scholar 

  85. Hussein, I. I., Schaub, H. Invariant shape solutions of the spinning three craft coulomb tether problem. Celestial Mechanics and Dynamical Astronomy, 2006, 96(2): 137–157.

    Article  MathSciNet  MATH  Google Scholar 

  86. Hussein, I., Schaub, H. Stability and control of relative equilibria for the three-spacecraft coulomb tether problem. Acta Astronautica, 2009, 65(5–6): 738–754.

    Article  Google Scholar 

  87. Schaub, H., Hussein, I. I. Stability and recon guration analysis of a circularly spinning two-craft coulomb tether. IEEE Transactions on Aerospace and Electronic Systems, 2010, 46(4): 1675–1686.

    Article  Google Scholar 

  88. Hogan, E. A., Schaub, H. Collinear invariant shapes for three-spacecraft coulomb formations. Acta Astronautica, 2012, 72: 78–89.

    Article  Google Scholar 

  89. Hogan, E. A., Schaub, H. Linear stability and shape analysis of spinning three-craft coulomb formations. Celestial Mechanics and Dynamical Astronomy, 2012, 112(2): 131–148.

    Article  MathSciNet  Google Scholar 

  90. Jasch, P. D., Hogan, E. A., Schaub, H. Out-of- plane stability analysis of collinear spinning three-craft coulomb formations. Acta Astronautica, 2013, 88: 89–97.

    Article  Google Scholar 

  91. Schaub, H., Jasper, L. E. Z. Orbit boosting maneuvers for two-craft coulomb formations. Journal of Guidance, Control, and Dynamics, 2013, 36(1): 74–82.

    Article  Google Scholar 

  92. Stevenson, D. Remote spacecraft attitude control by coulomb charging. Ph.D. Dissertation, University of Colorado at Boulder, Boulder, CO, 2015.

    Google Scholar 

  93. Shibata, T., Bennett, T., Schaub, H. Prospects of a hybrid magnetic/electrostatic sample container retriever. The 9th International Workshop on Satellite Constellations and Formation Flying, 2017.

    Google Scholar 

  94. Aslanov, V. S., Yudintsev, V. V. Relative motion control of space pusher-tug during debris removal by a coulomb force. Journal of Guidance, Control, and Dynamics, 2017.

    MATH  Google Scholar 

  95. Seubert, C. R., Schaub, H. Closed-loop charged relative motion experiments simulating constrained orbital motion. Journal of Guidance, Control, and Dynamics, 2010, 33(6): 1856–1865.

    Article  Google Scholar 

  96. Seubert, C. R., Schaub, H. Electrostatic force model for terrestrial experiments on the coulomb testbed. The 61st International Astronautical Congress, 2010.

    Google Scholar 

  97. Bennett, T., Schaub, H. Touchless electrostatic three- dimensional detumbling of large axi-symmetric debris. The Journal of the Astronautical Sciences, 2015, 62(3): 233–253.

    Article  Google Scholar 

  98. Bennett, T., Schaub, H. Capitalizing on relative motion in electrostatic detumble of axi-symmetric geo objects. The 6th International Conference on Astrodynamics Tools and Techniques, 2016.

    Google Scholar 

  99. Aslanov, V. S. Exact solutions and adiabatic invariants for equations of satellite attitude motion under coulomb torque. Nonlinear Dynamics, 2017, 90(4): 2545–2556.

    Article  MathSciNet  Google Scholar 

  100. Stevenson, D., Schaub, H. Terrestrial testbed for remote coulomb spacecraft rotation control. International Journal of Space Science and Engineering, 2014, 2(1): 96–112.

    Article  Google Scholar 

  101. Bennett, T., Stevenson, D., Hogan, E., McManus, L., Schaub, H. Prospects and challenges of touchless debris despinning using electrostatics. The 3rd European Workshop on Space Debris Modeling and Remediation, 2014.

    Google Scholar 

  102. Hogan, E. A., Schaub, H. Space debris reorbiting using electrostatic actuation. The 35th Annual Guidance and Control Conference, 2012.

    Google Scholar 

  103. Hughes, J., Schaub, H. Monte-carlo analysis of the pulsed electrostatic tractor strength. The 14th Spacecraft Charging Technology Conference, 2016.

    Google Scholar 

  104. Anderson, P. V., Schaub, H. Conjunction challenges of low-thrust geosynchronous debris removal maneuvers. Acta Astronautica, 2016, 123: 154–164.

    Article  Google Scholar 

  105. Bennett, T. J. On-orbit 3-dimensional electrostatic detumble for generic spacecraft geometries. Ph.D. Dissertation, University of Colorado at Boulder, Boulder, CO, 2017.

    Google Scholar 

  106. Ferguson, D. C., Murray-Krezan, J., Barton, D. A., Dennison, J. R., Gregory, S. A. Feasibility of detecting spacecraft charging and arcing by remote sensing. Journal of Spacecraft and Rockets, 2014, 51(6): 1907–1913.

    Article  Google Scholar 

  107. Engwerda, H. J. A., Hughes, J., Schaub, H. Remote sensing for planar electrostatic characterization using the multi-sphere method. Final Stardust Conference, 2016.

    Google Scholar 

  108. Engwerda, H. J. A. Remote sensing for spatial electrostatic characterization using the multi-sphere method. Master Dissertation, Delft University of Technology, Delft, The Netherlands, 2017.

    Google Scholar 

  109. Halekas, J. S., Mitchell, D. L., Lin, R. P., Hood, L. L., Acua, M. H., Binder, A. B. Evidence for negative charging of the lunar surface in shadow. Geophysical Research Letters, 2002, 29(10): 1435.

    Article  Google Scholar 

  110. Halekas, J. S., Delory, G. T., Lin, R. P., Stubbs, T. J., Farrell, W. M. Lunar prospector observations of the electrostatic potential of the lunar surface and its response to incident currents. Journal of Geophysical Research, 2008, 113(A9): A09102.

    Article  Google Scholar 

Download references

Author information

Authors and Affiliations

Authors

Corresponding author

Correspondence to M. Bengtson.

Additional information

Miles Bengtson is a graduate research assistant and NDSEG Fellow at the Aerospace Engineering Science Department, the University of Colorado, Boulder. He graduated with distinction with M.S. and B.S. degrees in engineering physics from Embry-Riddle Aeronautical University in Daytona Beach, FL. Miles is a space scholar at the Air Force Research Laboratory, an AIAA member, and an alumnus of the International Space University. His research interests include spacecraft-plasma interactions, charged astrodynamics, and experimentation.

Kieran Wilson is a graduate research assistant at the Autonomous Vehicle Systems (AVS) Laboratory of the University of Colorado, Boulder. He received his bachelor's degrees in aerospace and mechanical engineering from the University of Florida, in 2016. He has worked at Sandia National Laboratories, SpaceX, and Sierra Nevada Corporation. Research interests are in charged astrodynamics, formation flight, and spacecraft guidance, navigation, and control.

Joseph Hughes received his B.S. degrees in physics and mechanical engineering from Walla Walla University in College Place, WA and is now a PhD candidate at the University of Colorado Boulder at the Aerospace Engineering Sciences department. He has been awarded the John A. Vise award, the John V. Breakwell travel award, and has served as the Lead TA for the aerospace department. His current research interests include spacecraft charging, electrostatic force and torque estimation, and Coulomb astrodynamics.

Dr. Schaub is the Glenn L. Murphy Chair of Engineering at the University of Colorado and is the current graduate chair of the Aerospace Engineering Sciences department. He has over 20 years of research experience, of which 4 years are at Sandia National Laboratories. His research interests are in nonlinear dynamics and control, astrodynamics, relative motion dynamics, as well as relative motion sensing. This has led to about 137 journals and 208 conference publications, as well as a 3rd edition textbook on analytical mechanics of space systems. In the last decade, he has developed the emerging field of charged astrodynamics. Dr. Schaub has been the ADCS lead in the CICERO mission and the ADCS algorithm lead on a Mars mission. He has been awarded the H. Joseph Smead Faculty Fellowship, the Provosts Faculty Achievement Award, the faculty assembly award for excellence in teaching, as well as the Outstanding Faculty Advisor Award. He is an AAS fellow and AIAA associate fellow, and has won the AIAA/ASEE Atwood Educator Award, as well as the AIAA Mechanics and Control of Flight Award. He currently serves as the editor-in-chief for the AIAA Journal of Spacecraft and Rockets.

Rights and permissions

Reprints and permissions

About this article

Check for updates. Verify currency and authenticity via CrossMark

Cite this article

Bengtson, M., Wilson, K., Hughes, J. et al. Survey of the electrostatic tractor research for reorbiting passive GEO space objects. Astrodyn 2, 291–305 (2018). https://doi.org/10.1007/s42064-018-0030-0

Download citation

  • Received:

  • Accepted:

  • Published:

  • Issue Date:

  • DOI: https://doi.org/10.1007/s42064-018-0030-0

Keywords

Navigation