TY - GEN
T1 - High performance nap-of-the-earth unmanned helicopter flight
AU - Johnson, Eric N.
AU - Mooney, John G.
AU - Ong, Chester
AU - Sahasrabudhe, Vineet
AU - Hartman, Jonathan
PY - 2011/12/1
Y1 - 2011/12/1
N2 - This paper describes recent results from a partnership between the Sikorsky Aircraft Corporation and the Georgia Institute of Technology to develop, improve, and flight test a sensor, guidance, navigation, control, and real-time flight path optimization system to support high performance Nap-of-the-earth (NOE) helicopter flight. The emphasis here is on optimization for a combination of low height above terrain/obstacles and high speeds. Multiple methods for generating the desired flight path were evaluated, including (1) a simple processing of each laser scan; and (2) a potential field based method. Simulation and flight test results have been obtained utilizing an onboard laser scanner to detect terrain and obstacles while flying at low altitude, and have successfully demonstrated obstacle avoidance at speeds up to 40 ft/s while maintaining a miss distance of 50 ft horizontally and vertically. These results indicate that the technical approach is sound, paving the way for testing of even lower altitudes, higher speeds, and more aggressive maneuvering in future work.
AB - This paper describes recent results from a partnership between the Sikorsky Aircraft Corporation and the Georgia Institute of Technology to develop, improve, and flight test a sensor, guidance, navigation, control, and real-time flight path optimization system to support high performance Nap-of-the-earth (NOE) helicopter flight. The emphasis here is on optimization for a combination of low height above terrain/obstacles and high speeds. Multiple methods for generating the desired flight path were evaluated, including (1) a simple processing of each laser scan; and (2) a potential field based method. Simulation and flight test results have been obtained utilizing an onboard laser scanner to detect terrain and obstacles while flying at low altitude, and have successfully demonstrated obstacle avoidance at speeds up to 40 ft/s while maintaining a miss distance of 50 ft horizontally and vertically. These results indicate that the technical approach is sound, paving the way for testing of even lower altitudes, higher speeds, and more aggressive maneuvering in future work.
UR - http://www.scopus.com/inward/record.url?scp=84857880405&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=84857880405&partnerID=8YFLogxK
M3 - Conference contribution
AN - SCOPUS:84857880405
SN - 9781618393234
T3 - American Helicopter Society International - AHS Specialists' Meeting on Unmanned Rotorcraft and Network Centric Operations 2011
SP - 167
EP - 175
BT - American Helicopter Society International - AHS Specialists' Meeting on Unmanned Rotorcraft and Network Centric Operations 2011
T2 - AHS Specialists' Meeting on Unmanned Rotorcraft and Network Centric Operations 2011
Y2 - 25 January 2011 through 27 January 2011
ER -