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.
Application of guidance laws to quadrotor landing
01.06.2015
2383751 byte
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
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