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Ultra-Light Planetary Manipulator: Study and Development

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Aerospace Robotics

Abstract

The demand for the use of Planetary Manipulators is quite obvious in space exploration and in situ research. It can also be predicted that its role will expand in upcoming decades given the planned intensification of space exploration. This chapter presents the newly developed 3dof Ultra-Light Planetary Manipulator (ULPM) designated for extended servicing of exploration tools (e.g., penetrators, small rovers, etc.), or scientific instruments and sensors in planetary missions, where Mars and Moon are the mostly foreseen destinations. It combines new ideas and earlier achievements, both of which had influence on the concept and would demonstrate the technology. In consequence, a laboratory model device was successively developed. Two leading constraints determined the design: very low mass of the unit and long extension range of deployment of the servicing instruments. For those reasons, the utilization of the tubular boom mechanism was preferred. Integrated Ultra-Light Planetary Manipulator was tested in laboratory conditions in order to prove its operational functionality and performance. Particularly, it was examined what is the safety deployment distance for certain loads with acceptable stability of the flexible system structure. This topic was also one of the most important issues for performed analysis and manipulator’s dynamics simulations.

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References

  • Grygorczuk J, Banaszkiewicz M (1998) A concept study of the deployment device for the MUPUS penetrator on the Rosetta lander. (Rosetta –MUPUS, internal report)

    Google Scholar 

  • Grygorczuk J, Banaszkiewicz M, Seweryn K, Spohn T (2007) MUPUS insertion device for the Rosetta mission. J Telecommun Inf Technol 1:50–53

    Google Scholar 

  • Grygorczuk J, Banaszkiewicz M, Cichocki A, Ciesielska M, Dobrowolski M, Kędziora B, Krsowski J, Kuciński T, Marczewski M, Morawski M, Rickman H, Rybus T, Seweryn K, Skocki K, Spohn T, Szewczyk T, Wawrzaszek R, Wiśniewski Ł (2011) Advanced penetrators and hammering sampling devices for planetary body exploration. In: Proceedings of the 11th symposium on advanced space technologies in robotics and automation, ESA/ESTEC, Noordwijk

    Google Scholar 

  • Junkins J, Kim Y (1993) Introduction to dynamics and control of flexible structures. AIAA, Washington

    Book  Google Scholar 

  • Paulikas GA, Pieters CM, Banerdt WB, Burch JL, Chaikin A, Cohen BA, Duke M, England AW, Hiesinger H, Hinners NW, Howard AM, Lawrence DJ, Lester DF, Lucey PG, Stern SA, Tompkins S, Valero FPJ, Valley JW, Walker CD, Woolf NJ (2007) The scientific context for the exploration of the Moon. National Research Council, Washington

    Google Scholar 

  • Seweryn K, Banaszkiewicz M, Maediger B, Rybus T, Sommer J (2011) Dynamics of space robotic arm during interactions with non cooperative objects. In: Proceedings of 11th symposium on advanced space technologies in robotics and automation (ASTRA)

    Google Scholar 

  • Seweryn K, Grygorczuk J, Wawrzaszek R, Banaszkiewicz M, Rybus T, Wiśniewski Ł (2012) Low velocity penetrators (LVP) driven by hammering action—definition of the principle of operation based on numerical models and experimental tests. Submitted to mechanism and machine theory

    Google Scholar 

  • Smith A, Crawford IA, Gowen RA, Ball AJ, Barber SJ, Church P, Coates AJ, Gao Y, Griffiths AD, Hagermann A, Joy KH, Phipps A, Pike WT, Scott R, Sheridan S, Sweeting M, Talboys D, Tong V, Wells N, Biele J, Chela-Flores J, Dabrowski B, Flannagan J, Grande M, Grygorczuk J, Kargl G, Khavroshkin OB, Klingelhoefer G, Knapmeyer M, Marczewski W, McKenna-Lawlor S, Richter L, Rothery DA, Seweryn K, Ulamec S, Wawrzaszek R, Wieczorek M, Wright IP, Sims M (2009) Lunar EX—a proposal to cosmic vision. Exp Astron J. doi 10.1007/s10686-008-9109-6A

  • Spohn T, Seiferlin K, Hagermann A, Knollenberg J, Ball AJ, Banaszkiewicz M, Benkhoff J, Gadomski S, Gregorczuk W, Grygorczuk J, Hlond M, Kargl G, Kührt E, Kömle N, Krasowski J, Marczewski W, Zarnecki JC (2006) Muspus—a thermal and mechanical properties probe for the Rosetta Lander Philae. Space Sci Rev 128:339–362

    Article  Google Scholar 

  • Tsai L-W (1999) Robot analysis: the mechanics of serial and parallel manipulators. John Wiley & Sons, New York

    Google Scholar 

  • Wood G, Kennedy D (2003) Simulating mechanical systems in simulink with SimMechanics. Technical report 91124v00, The MathWorks, Inc., Natick

    Google Scholar 

Download references

Acknowledgments

The chapter was supported by the NCN project no N N514 234537.

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Correspondence to Jerzy Grygorczuk .

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Grygorczuk, J. et al. (2013). Ultra-Light Planetary Manipulator: Study and Development. In: Sąsiadek, J. (eds) Aerospace Robotics. GeoPlanet: Earth and Planetary Sciences. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-34020-8_11

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