Reachability analysis of landing sites for forced landing of a UAS in wind using trochoidal turn paths

Matthew Coombes, Wen Hua Chen, Peter Render

Research output: Chapter in book / Conference proceedingConference article published in proceeding or bookAcademic researchpeer-review

11 Citations (Scopus)

Abstract

This paper details a method to ascertain the reachability of known emergency landing sites for any fixed wing aircraft in a forced landing due to engine failure in steady uniform wind conditions. With knowledge of the aircraft's state and parameters, and landing site location and landing direction, the minimum height loss path can be defined. This uses glide performance calculations and a trajectory planner to give a minimum height loss to each landing site. Based on the aircraft's initial altitude it can calculate if the site is reachable, and how reachable it is. The path definition takes into account wind and uses a geometric shape called a trochoid to define the gliding turns in wind. This method is generic enough for use by any aircraft in any wind conditions.

Original languageEnglish
Title of host publication2015 International Conference on Unmanned Aircraft Systems, ICUAS 2015
PublisherInstitute of Electrical and Electronics Engineers Inc.
Pages62-71
Number of pages10
ISBN (Electronic)9781479960101
DOIs
Publication statusPublished - 7 Jul 2015
Event2015 International Conference on Unmanned Aircraft Systems, ICUAS 2015 - Denver, United States
Duration: 9 Jun 201512 Jun 2015

Publication series

Name2015 International Conference on Unmanned Aircraft Systems, ICUAS 2015

Conference

Conference2015 International Conference on Unmanned Aircraft Systems, ICUAS 2015
Country/TerritoryUnited States
CityDenver
Period9/06/1512/06/15

Keywords

  • Forced landings
  • Gliding
  • Reachability analysis
  • Trochoids

ASJC Scopus subject areas

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

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