Application of Guidance Laws to Quadrotor Landing Conference Paper

abstract

• 2015 IEEE. 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.

name of conference

• 2015 International Conference on Unmanned Aircraft Systems (ICUAS)

authors

• Saripalli, Srikanth

published proceedings

• 2015 INTERNATIONAL CONFERENCE ON UNMANNED AIRCRAFT SYSTEMS (ICUAS'15)

author list (cited authors)

• Gautam, A., Sujit, P. B., & Saripalli, S.

citation count

• 10

complete list of authors

• Gautam, Alvika||Sujit, PB||Saripalli, Srikanth

publication date

• June 2015

publisher

• Institute of Electrical and Electronics Engineers (IEEE)  Publisher

published in

• n2373-6720ISSN  Journal

Digital Object Identifier (DOI)

• 10.1109/icuas.2015.7152312

International Standard Book Number (ISBN) 13

• 9781479960101

start page

• 372

end page

• 379