Title :
Application of guidance laws to quadrotor landing
Author :
Gautam, Alvika ; Sujit, P.B. ; Saripalli, Srikanth
Abstract :
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.
Keywords :
Global Positioning System; autonomous aerial vehicles; missile guidance; GPS location; Matlab simulations; ROS implementation; aerial vehicle landing; guidance laws; line-of-sight guidance; missile guidance principles; pure proportional navigation guidance; pure pursuit guidance; quadrotor landing; Acceleration; Gold; MATLAB; Navigation; Three-dimensional displays; Trajectory; Vehicles;
Conference_Titel :
Unmanned Aircraft Systems (ICUAS), 2015 International Conference on
Conference_Location :
Denver, CO
Print_ISBN :
978-1-4799-6009-5
DOI :
10.1109/ICUAS.2015.7152312
