Application of guidance laws to quadrotor landing

Alvika Gautam, P. B. Sujit, Srikanth Saripalli

Research output: Chapter in Book/Report/Conference proceedingConference contribution

7 Scopus citations

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.

Original languageEnglish (US)
Title of host publication2015 International Conference on Unmanned Aircraft Systems, ICUAS 2015
PublisherInstitute of Electrical and Electronics Engineers Inc.
Pages372-379
Number of pages8
ISBN (Print)9781479960101
DOIs
StatePublished - Jul 7 2015
Event2015 International Conference on Unmanned Aircraft Systems, ICUAS 2015 - Denver, United States
Duration: Jun 9 2015Jun 12 2015

Other

Other2015 International Conference on Unmanned Aircraft Systems, ICUAS 2015
CountryUnited States
CityDenver
Period6/9/156/12/15

ASJC Scopus subject areas

  • Transportation
  • Aerospace Engineering
  • Control and Systems Engineering
  • Electrical and Electronic Engineering

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