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Robotics Institute Seminar, Friday, December 4, 1998
Robotics Institute Carnegie Mellon University Pittsburgh PA 15213-3891 412/268-8525 . 412/268-5576 (fax)
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Drilling for Lunar Ice: Rover and Lander Design for the Icebreaker Mission
Place and Time
Abstract Sorties into the permanently dark regions require navigation using teleoperation, limited range imaging, dead reckoning, track following, horizon landmarks, and 50 meter resolution global maps. The rover must traverse kilometers of temporary dark, enter the cold trap, drill, and return to the light to recharge. After many sorties during the approximately 350 hour lunar day, during which the sunlit area migrates from the west side of the crater to the east, the rover must end up near where it began, to position itself for the next lunar sunrise. As part of Red Whittaker's Mobile Robot Design Course, a group of 12 students undertook the design of a lunar rover and lander for the Icebreaker mission. During this seminar, they will present their work, which has been reviewed by the aerospace industry.
Speaker Biography Two members of the design team have space industry experience in mechanism and structural design (JPL, Pathfinder), and astrodynamics (Hughes Communications). Others have first-hand experience in robotics systems (Pandora), GNC (Nomad), and computation. Throughout the semester the design team, with external contributors and reviewers from around the country, have iterated upon the design of a viable lunar rover/lander system. The result is a 90 kg rover capable of surviving the severe lunar environment of dust, radiation, and extreme temperatures.
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