Design, modeling and tuning of modified PID controller for autopilot in MAVs

Xu Hui Chen; Ejaz Ul Haq; Jiawei Lin

doi:10.1109/SNPD.2016.7515943

Design, modeling and tuning of modified PID controller for autopilot in MAVs

Xu Hui Chen
, Ejaz Ul Haq
, Jiawei Lin

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

5 Scopus citations

Abstract

The dangers of poor pilot performance as well as time and place conditions, low altitude and climate, damage critical aircraft control system. The use of Unmanned Aircraft Vehicle or (UAV) in sensitive and important Operation is required and there is a need for autopilot that can tune the MAV in different environment conditions. Furthermore, designing the controller system is one of the main discussed Dynamic issues in Flying Objects. In this paper an attempted is made to determine the optimal coefficients of PID controller that can reject disturbances and still operate the MAV in stable positions. Basic PID controller is designed and is adopted to control the MAV, a modified techniques incorporating ISA-PID is designed to reject disturbances. The PID parameters are determined to be reduce the rise time less than 3 seconds, settling time to be less than 8 seconds and overshoot to be less than 5%. The developed model is suitable for PID controller in autopilot.

Original language	English
Title of host publication	2016 IEEE/ACIS 17th International Conference on Software Engineering, Artificial Intelligence, Networking and Parallel/Distributed Computing, SNPD 2016
Editors	Yihai Chen
Publisher	Institute of Electrical and Electronics Engineers Inc.
Pages	475-480
Number of pages	6
ISBN (Electronic)	9781509022397
DOIs	https://doi.org/10.1109/SNPD.2016.7515943
State	Published - 18 Jul 2016
Externally published	Yes
Event	17th IEEE/ACIS International Conference on Software Engineering, Artificial Intelligence, Networking and Parallel/Distributed Computing, SNPD 2016 - Shanghai, China Duration: 30 May 2016 → 1 Jun 2016

Publication series

Name	2016 IEEE/ACIS 17th International Conference on Software Engineering, Artificial Intelligence, Networking and Parallel/Distributed Computing, SNPD 2016

Conference

Conference	17th IEEE/ACIS International Conference on Software Engineering, Artificial Intelligence, Networking and Parallel/Distributed Computing, SNPD 2016
Country/Territory	China
City	Shanghai
Period	30/05/16 → 1/06/16

Bibliographical note

Publisher Copyright:
© 2016 IEEE.

Keywords

ISA-PID
MAV
PID controller
Unmanned Aircraft Vehicle
autopilot

ASJC Scopus subject areas

Artificial Intelligence
Computer Networks and Communications
Software

Access to Document

10.1109/SNPD.2016.7515943

Cite this

Chen, X. H., Haq, E. U., & Lin, J. (2016). Design, modeling and tuning of modified PID controller for autopilot in MAVs. In Y. Chen (Ed.), 2016 IEEE/ACIS 17th International Conference on Software Engineering, Artificial Intelligence, Networking and Parallel/Distributed Computing, SNPD 2016 (pp. 475-480). Article 7515943 (2016 IEEE/ACIS 17th International Conference on Software Engineering, Artificial Intelligence, Networking and Parallel/Distributed Computing, SNPD 2016). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/SNPD.2016.7515943

Chen, Xu Hui ; Haq, Ejaz Ul ; Lin, Jiawei. / Design, modeling and tuning of modified PID controller for autopilot in MAVs. 2016 IEEE/ACIS 17th International Conference on Software Engineering, Artificial Intelligence, Networking and Parallel/Distributed Computing, SNPD 2016. editor / Yihai Chen. Institute of Electrical and Electronics Engineers Inc., 2016. pp. 475-480 (2016 IEEE/ACIS 17th International Conference on Software Engineering, Artificial Intelligence, Networking and Parallel/Distributed Computing, SNPD 2016).

@inproceedings{c6f88d257c1840aaa76bae1d53a1a998,

title = "Design, modeling and tuning of modified PID controller for autopilot in MAVs",

abstract = "The dangers of poor pilot performance as well as time and place conditions, low altitude and climate, damage critical aircraft control system. The use of Unmanned Aircraft Vehicle or (UAV) in sensitive and important Operation is required and there is a need for autopilot that can tune the MAV in different environment conditions. Furthermore, designing the controller system is one of the main discussed Dynamic issues in Flying Objects. In this paper an attempted is made to determine the optimal coefficients of PID controller that can reject disturbances and still operate the MAV in stable positions. Basic PID controller is designed and is adopted to control the MAV, a modified techniques incorporating ISA-PID is designed to reject disturbances. The PID parameters are determined to be reduce the rise time less than 3 seconds, settling time to be less than 8 seconds and overshoot to be less than 5\%. The developed model is suitable for PID controller in autopilot.",

keywords = "ISA-PID, MAV, PID controller, Unmanned Aircraft Vehicle, autopilot",

author = "Chen, \{Xu Hui\} and Haq, \{Ejaz Ul\} and Jiawei Lin",

note = "Publisher Copyright: {\textcopyright} 2016 IEEE.; 17th IEEE/ACIS International Conference on Software Engineering, Artificial Intelligence, Networking and Parallel/Distributed Computing, SNPD 2016 ; Conference date: 30-05-2016 Through 01-06-2016",

year = "2016",

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doi = "10.1109/SNPD.2016.7515943",

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series = "2016 IEEE/ACIS 17th International Conference on Software Engineering, Artificial Intelligence, Networking and Parallel/Distributed Computing, SNPD 2016",

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Chen, XH, Haq, EU & Lin, J 2016, Design, modeling and tuning of modified PID controller for autopilot in MAVs. in Y Chen (ed.), 2016 IEEE/ACIS 17th International Conference on Software Engineering, Artificial Intelligence, Networking and Parallel/Distributed Computing, SNPD 2016., 7515943, 2016 IEEE/ACIS 17th International Conference on Software Engineering, Artificial Intelligence, Networking and Parallel/Distributed Computing, SNPD 2016, Institute of Electrical and Electronics Engineers Inc., pp. 475-480, 17th IEEE/ACIS International Conference on Software Engineering, Artificial Intelligence, Networking and Parallel/Distributed Computing, SNPD 2016, Shanghai, China, 30/05/16. https://doi.org/10.1109/SNPD.2016.7515943

Design, modeling and tuning of modified PID controller for autopilot in MAVs. / Chen, Xu Hui; Haq, Ejaz Ul; Lin, Jiawei.
2016 IEEE/ACIS 17th International Conference on Software Engineering, Artificial Intelligence, Networking and Parallel/Distributed Computing, SNPD 2016. ed. / Yihai Chen. Institute of Electrical and Electronics Engineers Inc., 2016. p. 475-480 7515943 (2016 IEEE/ACIS 17th International Conference on Software Engineering, Artificial Intelligence, Networking and Parallel/Distributed Computing, SNPD 2016).

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

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N2 - The dangers of poor pilot performance as well as time and place conditions, low altitude and climate, damage critical aircraft control system. The use of Unmanned Aircraft Vehicle or (UAV) in sensitive and important Operation is required and there is a need for autopilot that can tune the MAV in different environment conditions. Furthermore, designing the controller system is one of the main discussed Dynamic issues in Flying Objects. In this paper an attempted is made to determine the optimal coefficients of PID controller that can reject disturbances and still operate the MAV in stable positions. Basic PID controller is designed and is adopted to control the MAV, a modified techniques incorporating ISA-PID is designed to reject disturbances. The PID parameters are determined to be reduce the rise time less than 3 seconds, settling time to be less than 8 seconds and overshoot to be less than 5%. The developed model is suitable for PID controller in autopilot.

AB - The dangers of poor pilot performance as well as time and place conditions, low altitude and climate, damage critical aircraft control system. The use of Unmanned Aircraft Vehicle or (UAV) in sensitive and important Operation is required and there is a need for autopilot that can tune the MAV in different environment conditions. Furthermore, designing the controller system is one of the main discussed Dynamic issues in Flying Objects. In this paper an attempted is made to determine the optimal coefficients of PID controller that can reject disturbances and still operate the MAV in stable positions. Basic PID controller is designed and is adopted to control the MAV, a modified techniques incorporating ISA-PID is designed to reject disturbances. The PID parameters are determined to be reduce the rise time less than 3 seconds, settling time to be less than 8 seconds and overshoot to be less than 5%. The developed model is suitable for PID controller in autopilot.

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ER -

Chen XH, Haq EU, Lin J. Design, modeling and tuning of modified PID controller for autopilot in MAVs. In Chen Y, editor, 2016 IEEE/ACIS 17th International Conference on Software Engineering, Artificial Intelligence, Networking and Parallel/Distributed Computing, SNPD 2016. Institute of Electrical and Electronics Engineers Inc. 2016. p. 475-480. 7515943. (2016 IEEE/ACIS 17th International Conference on Software Engineering, Artificial Intelligence, Networking and Parallel/Distributed Computing, SNPD 2016). doi: 10.1109/SNPD.2016.7515943

Design, modeling and tuning of modified PID controller for autopilot in MAVs

Abstract

Publication series

Conference

Bibliographical note

Keywords

ASJC Scopus subject areas

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