Fundamental numerical and experimental evaluation of attitude recovery control for a quad tilt rotor UAV against disturbance

Satoko Abiko, Kengo Tashiro

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

  • 1 Citations

Abstract

This paper presents attitude recovery control for a quad tilt rotor UAV. The quad tilt rotor UAV has ability of flying with completely independent 3 DOF position and 3 DOF attitude control by changing the thrust directions. This type of UAV is expected to perform better response to the disturbance by virtue of the mechanism of changing the thrust directions compared to the conventional multi-rotor UAV. This paper proposes disturbance detection method using IMU sensor and develops attitude recovery control against impact disturbance. The numerical simulation and fundamental flight experiments were carried out to evaluate the effectiveness of the proposed method compared to the conventional PID control.

LanguageEnglish
Title of host publicationICCAS 2016 - 2016 16th International Conference on Control, Automation and Systems, Proceedings
PublisherIEEE Computer Society
Pages709-712
Number of pages4
ISBN (Electronic)9788993215120
DOIs
StatePublished - 2017 Jan 24
Event16th International Conference on Control, Automation and Systems, ICCAS 2016 - Gyeongju, Korea, Republic of
Duration: 2016 Oct 162016 Oct 19

Other

Other16th International Conference on Control, Automation and Systems, ICCAS 2016
CountryKorea, Republic of
CityGyeongju
Period16/10/1616/10/19

Fingerprint

Unmanned aerial vehicles (UAV)
Rotors
Recovery
Three term control systems
Attitude control
Sensors
Computer simulation
Experiments

Keywords

  • Attitude recovery flight
  • Impact disturbance
  • Tilt rotor aircraft
  • Unmanned Aerial Vehicle (UAV)

ASJC Scopus subject areas

  • Artificial Intelligence
  • Computer Science Applications
  • Control and Systems Engineering
  • Electrical and Electronic Engineering

Cite this

Abiko, S., & Tashiro, K. (2017). Fundamental numerical and experimental evaluation of attitude recovery control for a quad tilt rotor UAV against disturbance. In ICCAS 2016 - 2016 16th International Conference on Control, Automation and Systems, Proceedings (pp. 709-712). [7832396] IEEE Computer Society. DOI: 10.1109/ICCAS.2016.7832396

Fundamental numerical and experimental evaluation of attitude recovery control for a quad tilt rotor UAV against disturbance. / Abiko, Satoko; Tashiro, Kengo.

ICCAS 2016 - 2016 16th International Conference on Control, Automation and Systems, Proceedings. IEEE Computer Society, 2017. p. 709-712 7832396.

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

Abiko, S & Tashiro, K 2017, Fundamental numerical and experimental evaluation of attitude recovery control for a quad tilt rotor UAV against disturbance. in ICCAS 2016 - 2016 16th International Conference on Control, Automation and Systems, Proceedings., 7832396, IEEE Computer Society, pp. 709-712, 16th International Conference on Control, Automation and Systems, ICCAS 2016, Gyeongju, Korea, Republic of, 16/10/16. DOI: 10.1109/ICCAS.2016.7832396
Abiko S, Tashiro K. Fundamental numerical and experimental evaluation of attitude recovery control for a quad tilt rotor UAV against disturbance. In ICCAS 2016 - 2016 16th International Conference on Control, Automation and Systems, Proceedings. IEEE Computer Society. 2017. p. 709-712. 7832396. Available from, DOI: 10.1109/ICCAS.2016.7832396
Abiko, Satoko ; Tashiro, Kengo. / Fundamental numerical and experimental evaluation of attitude recovery control for a quad tilt rotor UAV against disturbance. ICCAS 2016 - 2016 16th International Conference on Control, Automation and Systems, Proceedings. IEEE Computer Society, 2017. pp. 709-712
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