TY - GEN
T1 - Application of guidance laws to quadrotor landing
AU - Gautam, Alvika
AU - Sujit, P. B.
AU - Saripalli, Srikanth
N1 - Publisher Copyright:
© 2015 IEEE.
PY - 2015/7/7
Y1 - 2015/7/7
N2 - Aerial vehicle landing is an open and challenging problem. This paper focuses on development of simple guidance laws for quadrotor landing with known GPS location - stationary and moving. The guidance laws are based on missile guidance principles, namely pure pursuit, line-of-sight, and pure proportional navigation. Comparison on the performance of these guidance laws is presented through Matlab simulations and ROS implementation.
AB - Aerial vehicle landing is an open and challenging problem. This paper focuses on development of simple guidance laws for quadrotor landing with known GPS location - stationary and moving. The guidance laws are based on missile guidance principles, namely pure pursuit, line-of-sight, and pure proportional navigation. Comparison on the performance of these guidance laws is presented through Matlab simulations and ROS implementation.
UR - http://www.scopus.com/inward/record.url?scp=84941096955&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=84941096955&partnerID=8YFLogxK
U2 - 10.1109/ICUAS.2015.7152312
DO - 10.1109/ICUAS.2015.7152312
M3 - Conference contribution
AN - SCOPUS:84941096955
T3 - 2015 International Conference on Unmanned Aircraft Systems, ICUAS 2015
SP - 372
EP - 379
BT - 2015 International Conference on Unmanned Aircraft Systems, ICUAS 2015
PB - Institute of Electrical and Electronics Engineers Inc.
T2 - 2015 International Conference on Unmanned Aircraft Systems, ICUAS 2015
Y2 - 9 June 2015 through 12 June 2015
ER -