Keynote Speech 1

Keynote title:

Research on Novel Landing Mechanisms for Their Implementation in Lunar/Planetary Exploration Spacecraft in the Near Future

Abstract

Currently to suppress the effects of impacts on landing of lunar/planetary exploration spacecraft, most devices use the process of plastic deformation of the cushioning material similar to bumpers on an automobile. The body of the landing probe of Apollo’s lunar lander also suppressed impact by using plastic deformation in a honeycomb design. However, in order to obtain highly reliable mechanisms at low costs, a shock response control mechanism that can be re-experimented on is necessary, instead of a crushing shock suppression mechanism. For this purpose, we have proposed two ideas and their applicable mechanisms – the momentum exchange type and the energy exchange type. This talk introduces the effectiveness and features of the methodologies based on these two ideas.

  Biography

Prof. Susumu Hara (Senior Member, IEEE) received the B.S., M.S., and Ph.D. degrees in engineering from Keio University, Tokyo, Japan, in 1992, 1994, and 1996, respectively. From 1995 to 2000, he was a Research Fellow with the Japan Society for the Promotion of Science. From 1996 to 2000, he was a Visiting Researcher with the Faculty of Science and Technology, Keio University. From 1998 to 1999, he was a Visiting Scholar with the Department of Mechanical Engineering, University of California at Berkeley, Berkeley, CA, USA. In 2000, he joined the Faculty of the Toyota Technological Institute, Nagoya, Japan. In 2008, he joined the Faculty of Nagoya University, Nagoya, where he is currently a Professor with the Department of Aerospace Engineering, Graduate School of Engineering. His current research interests include motion and vibration control of mechanical structures, nonstationary control methods, control problems of man-machine systems, and aerospace equipment.