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Sponsors: NASA Ames Research Center NASA Idaho Space Grant - PowerPoint PPT Presentation

Sponsors: NASA Ames Research Center NASA Idaho Space Grant Consortium University of Idaho College of Engineering Graduate Fellow: Aaron Goodin Joined the RLEP team as a ME undergrad in the Capstone Design Program at the


  1. Sponsors: NASA Ames Research Center � NASA Idaho Space Grant Consortium � University of Idaho College of Engineering � Graduate Fellow: Aaron Goodin

  2. � Joined the RLEP team as a ME undergrad in the Capstone Design Program at the University of Idaho. � Tasked with a project to create a non- prehensile robotic manipulator to accomplish multiple tasks outlined by the Intelligent Robotics Group at NASA ARC � Initial goal was to adapt to IRG’s K10 rover

  3. � Soil Sample Collection Trenching � � Dislodging K-10 Rover Cable Laying � � Rock Chipping � Soil Compaction Path Clearing � Soil Relocating � � Rock Flipping Rock Pushing � Soil Sifting � Tilling � Stake Planting �

  4. Linear Actuator Elbow Rotation Shoulder Rotation Electronic Hardware Base Rotation

  5. � Able to work on multi-disciplinary projects (ME, EE, CompE, CS) � Integrating multiple designs into one final package that has to work � Robotics = Motors � In-depth motor research � Motor Control � Micro processing & Programming � Applying CAD for a real purpose � Spending time in the machine shop learning important manufacturing principles � Working with a team!!! not always easy

  6. � Applied for ISGC fellowship and became the next RLEP fellow. � Traveled to NASA ARC for the first summer internship. � Mentored in the design and fabrication of the second RLEP robotic platform.

  7. � Gained project management experience by co- managing a team of Robotics Academy Students to improve L07 � Mentored students to help them in the design process � Worked to specify the next RLEP project

  8. Old Interface New and Improved Interface Improvement Areas: • Easier navigation between joint control • More control options • Incorporate real time video • Programmed Stop command

  9. Old Avionics New Avionics Brushless XP-08 Power DC123S DC motor Management Converter Controller DC1HV DC Wireless Kill BS2 Board of DC Motor Converter Switch Education Controller Servo Motor Controller 16 volt Lithium Mini ITX board Basic Stamps Motor Mind 12 volt Power 6 volt Power Ion Batteries Controller Supply Supply Boards Wiring done by Jennifer Allen

  10. Cam/Follower poker design used for Base Design for 3-phase direct drive percussive pecking motor Bearing Mounting Frame Fastener Motor Rotor Mounting Frame Motor Stator Base Frame Greatly Improved Avionics Box

  11. � Project management experience � Learning to delegate � Learning to manage: i.e. problematic team members � Advanced machining capabilities � Presentations, Publishing's, Networking, and more � Leveraging � Experiences � Great research opportunities � NASA related research � Lunar Science Institute � RLEP related research � Robots going to The Moon � My Thesis work � NASA + RLEP = MSME � Bio-Tensegrity

  12. • a continuous TENSION network structured by discontinuous COMPRESSION members. • Tension members must be pre ‐ stressed and will never go into compression. • No Bending or Shear stresses!!!

  13. R. BUCKMINSTER FULLER KENNETH SNELSON � Architect and Inventor � Artist � Coined the term � Known as the “Father of Tensegrity by joining Tensegrity” the terms: “Tension” & “Structural Integrity” Fuller Dome: Snelson’s Tower: Geodesic Dome Needle Tower

  14. • Five shapes are said to enable the construction of tensegrity structures • All of these shapes are based off of the equilateral triangle Tetrahedron Octahedron Dodecahedron Icosahedron

  15. Max: 9,600 N Calculated: 36,000N

  16. Tom Flemmons – Fascia – • The soft connective • Began designing and tissue in the body building bio- comprised of tendons, tensegrity structures ligaments, and cartilage in the 1970’s • Uninterrupted, three- dimensional web of tissue that extends from head to toe.

  17. • ANDREW O. PAYNE FROM FLUIDIC ACTUATORS LIFT ARCHITECTS Airics Arm VIDEO

  18. DEPLOYABLE STRESS ANALYSIS FOR SIMPLE TENSEGRITIES TENSEGRITY STRUCTURES. � Tensegrity Structures � Use rods with given excel at taking area, length, and unknown force vectors material properties and distributing the � Apply loads with a stress efficiently known direction and � Could be used to magnitude package instruments � Using strain gauges to being deployed that will take loads from any measure stress at direction of unknown multiple points on rods magnitude.

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