DocumentCode
3074219
Title
Application of guidance laws to quadrotor landing
Author
Gautam, Alvika ; Sujit, P.B. ; Saripalli, Srikanth
fYear
2015
fDate
9-12 June 2015
Firstpage
372
Lastpage
379
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;
fLanguage
English
Publisher
ieee
Conference_Titel
Unmanned Aircraft Systems (ICUAS), 2015 International Conference on
Conference_Location
Denver, CO
Print_ISBN
978-1-4799-6009-5
Type
conf
DOI
10.1109/ICUAS.2015.7152312
Filename
7152312
Link To Document