Supervisory fault tolerant control of the NASA AirStar aircraft

Tamás Péni, Bálint Vanek, Z. Szabó, J. Bokor

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

7 Citations (Scopus)

Abstract

A multi-level reconfiguration framework is proposed for fault tolerant control of overactuated aerial vehicles, where the levels indicate how much authority is given to the reconfiguration task. On the lowest, first level the fault is accommodated by modifying only the actuator/sensor configuration, so the fault remains hidden from the baseline controller. A dynamic reallocation scheme is applied on this level. The allocation mechanism exploits the actuator/sensor redundancy available on the aircraft. In case the fault cannot be managed at the actuator/sensor level the reconfiguration process has access the baseline controller. Based on the LPV control framework, this is done by introducing fault-specific scheduling parameters. The baseline controller is designed to provide acceptable performance level along all fault scenarios coded in these scheduling variables. The decision of which reconfiguration level has to be initiated in response to a fault is determined by a supervisor unit. The method is demonstrated on the full six degrees of freedom nonlinear simulation model of the GTM UAV.

Original languageEnglish
Title of host publicationProceedings of the American Control Conference
PublisherInstitute of Electrical and Electronics Engineers Inc.
Pages666-671
Number of pages6
ISBN (Print)9781479932726
DOIs
Publication statusPublished - 2014
Event2014 American Control Conference, ACC 2014 - Portland, OR, United States
Duration: Jun 4 2014Jun 6 2014

Other

Other2014 American Control Conference, ACC 2014
CountryUnited States
CityPortland, OR
Period6/4/146/6/14

Fingerprint

NASA
Actuators
Aircraft
Controllers
Sensors
Scheduling
Supervisory personnel
Unmanned aerial vehicles (UAV)
Redundancy
Antennas

Keywords

  • Fault-tolerant systems
  • Flight control
  • Supervisory control

ASJC Scopus subject areas

  • Electrical and Electronic Engineering

Cite this

Péni, T., Vanek, B., Szabó, Z., & Bokor, J. (2014). Supervisory fault tolerant control of the NASA AirStar aircraft. In Proceedings of the American Control Conference (pp. 666-671). [6859264] Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/ACC.2014.6859264

Supervisory fault tolerant control of the NASA AirStar aircraft. / Péni, Tamás; Vanek, Bálint; Szabó, Z.; Bokor, J.

Proceedings of the American Control Conference. Institute of Electrical and Electronics Engineers Inc., 2014. p. 666-671 6859264.

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

Péni, T, Vanek, B, Szabó, Z & Bokor, J 2014, Supervisory fault tolerant control of the NASA AirStar aircraft. in Proceedings of the American Control Conference., 6859264, Institute of Electrical and Electronics Engineers Inc., pp. 666-671, 2014 American Control Conference, ACC 2014, Portland, OR, United States, 6/4/14. https://doi.org/10.1109/ACC.2014.6859264
Péni T, Vanek B, Szabó Z, Bokor J. Supervisory fault tolerant control of the NASA AirStar aircraft. In Proceedings of the American Control Conference. Institute of Electrical and Electronics Engineers Inc. 2014. p. 666-671. 6859264 https://doi.org/10.1109/ACC.2014.6859264
Péni, Tamás ; Vanek, Bálint ; Szabó, Z. ; Bokor, J. / Supervisory fault tolerant control of the NASA AirStar aircraft. Proceedings of the American Control Conference. Institute of Electrical and Electronics Engineers Inc., 2014. pp. 666-671
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