Helicopter Statistics
| Body Size | 60 |
| Body Length | 62 inches |
| Rotor Diameter | 61 inches |
| Overall Weight | 46 pounds |
| Engine Size | 2.76 cubic inches |
| Engine Power | 4.75 HP |
| Navigational Sensors | TANS 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
Personnel
Team Members
Past Members
For comments or questions contact:
heli@sun-valley.stanford.edu
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