Flight testing of control allocation for elevator actuator fault in small UAV

Zulhilmy Sahwee, Aina Suriani Mahmood, Nazaruddin Abd Rahman, Khairul Salleh Mohamed Sahari

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

2 Citations (Scopus)

Abstract

Final validation of new control technique for any air vehicle must be conducted through flight testing. It is the most critical phase of the research work where it validates and provides real world feedback on the theoretical and simulation design. On the other hand, an unmanned aircraft as presented in this work is highly complex systems; a single component failure can lead to potentially dangerous consequences. The objective of this paper is to present the flight test result on the investigation on using alternate control surface for a control allocation of pitch control transition from elevator to stabilator of a small UAV. There were fourty flight tests have been performed and from the analysis, the proposed method is feasible to be used without affecting flight endurance and characteristics during flight control transition. The alternate control surface accommodation technique proves to promise higher reliability in case of faulty on-board actuator.

Original languageEnglish
Title of host publication2016 International Conference on Control, Automation and Information Sciences, ICCAIS 2016
PublisherInstitute of Electrical and Electronics Engineers Inc.
Pages232-237
Number of pages6
ISBN (Electronic)9781509006502
DOIs
Publication statusPublished - 17 Jan 2017
Event5th International Conference on Control, Automation and Information Sciences, ICCAIS 2016 - Ansan, Korea, Republic of
Duration: 27 Oct 201629 Oct 2016

Publication series

Name2016 International Conference on Control, Automation and Information Sciences, ICCAIS 2016

Other

Other5th International Conference on Control, Automation and Information Sciences, ICCAIS 2016
CountryKorea, Republic of
CityAnsan
Period27/10/1629/10/16

All Science Journal Classification (ASJC) codes

  • Computer Networks and Communications
  • Information Systems
  • Control and Systems Engineering
  • Control and Optimization

Fingerprint Dive into the research topics of 'Flight testing of control allocation for elevator actuator fault in small UAV'. Together they form a unique fingerprint.

  • Cite this

    Sahwee, Z., Mahmood, A. S., Abd Rahman, N., & Mohamed Sahari, K. S. (2017). Flight testing of control allocation for elevator actuator fault in small UAV. In 2016 International Conference on Control, Automation and Information Sciences, ICCAIS 2016 (pp. 232-237). [7822466] (2016 International Conference on Control, Automation and Information Sciences, ICCAIS 2016). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/ICCAIS.2016.7822466