Reverse engineering of a fixed wing unmanned aircraft 6-DoF model for navigation and guidance applications

Martin T. Burston, Roberto Sabatini, Reece Clothier, Alessandro Gardi, Subramanian Ramasamy

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

14 Scopus citations

Abstract

A method for deriving the parameters of a six-degree-of-freedom (6-DoF) aircraft dynamics model by adopting reverse engineering techniques is presented. The novelty of the paper is the adaption of the 6-DoF Aircraft Dynamics Model (ADM) as a virtual sensor integrated in a low-cost navigation and guidance system designed for small Unmanned Aircraft (UA). The mass and aerodynamic properties of the JAVELIN UA are determined with the aid of an accurate 3D scanning and CAD processing. For qualitatively assessing the calculated ADM, a trajectory with high dynamics is simulated for the JAVELIN UA and compared with that of a published 6-DoF model of the AEROSONDE UA. Additionally, to confirm the validity of the approach, reverse engineering procedures are applied to a published CAD model of the AEROSONDE UA aiding to the calculation of the associated 6-DoF model parameters. A spiral descent trajectory is generated using both the published and calculated parameters of the AEROSONDE UA and a comparative analysis is performed that validates the methodology. The accurate knowledge of the ADM is then utilized in the development of a virtual sensor to augment the UA navigation and guidance system in case of primary navigation sensor outages.

Original languageBritish English
Title of host publicationAEROTECH V
Subtitle of host publicationProgressive Aerospace Research
EditorsFairuz I. Romli, D.L. Majid, Faizal Mustapha, Fairuz I. Romli, D.L. Majid, Faizal Mustapha, Renuganth Varatharajoo, Fairuz I. Romli, Kamarul Arifin Ahmad, D.L. Majid, Faizal Mustapha, Renuganth Varatharajoo, Fairuz I. Romli, Kamarul Arifin Ahmad, D.L. Majid, Faizal Mustapha
Pages164-169
Number of pages6
ISBN (Electronic)9783038352327, 9783038352327
DOIs
StatePublished - 2014
Event5th AEROTECH conference - Kuala Lumpur, Malaysia
Duration: 29 Oct 201430 Oct 2014

Publication series

NameApplied Mechanics and Materials
Volume629
ISSN (Print)1660-9336
ISSN (Electronic)1662-7482

Conference

Conference5th AEROTECH conference
Country/TerritoryMalaysia
CityKuala Lumpur
Period29/10/1430/10/14

Keywords

  • 6-DoF
  • Flight dynamics
  • Laser scanner
  • Navigation and guidance system
  • Reverse engineering
  • Unmanned aircraft

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