Helicopter Statistics

Body Size60
Body Length62 inches
Rotor Diameter61 inches
Overall Weight46 pounds
Engine Size2.76 cubic inches
Engine Power4.75 HP
Navigational SensorsTANS Vector Differential Carrier Phase GPS


Current Capabilities

  • Dynamic Target Tracking and Following
  • Servoing from Vision Feedback
  • Autonomous Hover, Trajectory Following, and Landing
  • Object Location and Identification using Vision
  • Ferromagnetic Disk Retrieval

Future Capabilities

  • Autonomous Take-Offs
  • Parallel Camera Stereo Vision
  • Motion-Based Stereo Vision
  • Real-Time User Interaction
  • Human-Robot Team Mission Tasks

Global Positioning System

One of the greatest problems with controlling an autonomous helicopter is sensing position and attitude. Since a small, inexpensive vehicle is being used, it has neither the payload nor the financial budget to use exceedingly high quality inertial guidance systems. Navigation using differential carrier phase Global Positioning System (DCPGPS), is an active area of research within ARL, and offers an practical solution to these problems.

The Global Positioning System is an excellent sensor offering a wide variety of configurations. In its normal civilian configuration, it provides accuracies of roughly 100 meters in both position and altitude. Various (mainly differential) methods have been proposed and implemented for increasing this precision to about a meter. Stanford's use of carrier phase measurements allow accuracy on the order of centimeters. When carrier phase techniques are used in conjunction with multiple antenna, vehicle attitude can also be determined.


Publications

JonesFWR:1998 Conway:95
    GZipped Postscript 1766Kb
    PDF 3.0 1465Kb
    Andrew R. Conway.
    Autonomous Control of an Unstable Helicopter Using Carrier Phase GPS Only.
    PhD thesis, Stanford University, Stanford, CA 94305, March 1995.
    Also published as SUDAAR 664.
WoodleyJCR:95
    Postscript 679Kb
    GZipped Postscript 183Kb
    PDF 3.0 147Kb
    B. Woodley, C. Jennings, A. Conway, S. Rock.
    A Contestant in the 1995 International Aerial Robotics Competition. Aeroapce Robotics Laboratory Stanford University.
    Proceedings Manual. AUVS '95 Technical Papers, Washington DC, July 1995.
WoodleyJFLR:96
    Postscript 118Kb
    GZipped Postscript 32Kb
    PDF 3.0 95Kb
    B. Woodley, H. Jones, E. Frew, E. LeMaster, S. Rock.
    A Contestant in the 1996 International Aerial Robotics Competition. Aeroapce Robotics Laboratory Stanford University.
    AUVSI '96 Proceedings, Orlando, FL, July 1996.
WoodleyJLFR:96b WoodleyJFLR:97
    Postscript 339Kb
    GZipped Postscript 60Kb
    PDF 3.0 121Kb
    B. Woodley, H. Jones, E. Frew, E. LeMaster, S. Rock.
    A Contestant in the 1997 International Aerial Robotics Competition. Aeroapce Robotics Laboratory Stanford University.
    AUVSI '97 Proceedings, July 1997.

Personnel

Team Members

Past Members


For comments or questions contact: heli@sun-valley.stanford.edu