Experimental evaluation of PID and ESO controller for instrument landing system

Rahul Kumar Jain; Prashanth Kumar Shetty; Satyanarayan Shenoy

doi:10.1109/ICCICCT.2014.6993059

Experimental evaluation of PID and ESO controller for instrument landing system

Rahul Kumar Jain, Prashanth Kumar Shetty, Satyanarayan Shenoy

Manipal School of Information Sciences, Manipal

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

1 Citation (Scopus)

Abstract

This paper presents methodologies for design and experimental evaluation of both Proportional Integral and Derivative (PID) and Extended State Observer (ESO) controller for auto landing system. The process of auto landing can be experimentally described as second-order model for ES O controller. A PID controller and ES O controller is proposed to achieve the desired response for the autoland system. Computer simulations are performed to illustrate the performance of PID and ES O controller in comparison to each other. The applicability and usefulness of the proposed control scheme are well exemplified by conducting experiments on an aircraft model. Both simulations and experimental results reveal that the proposed PID and ES O scheme performs equally.

Original language	English
Title of host publication	2014 International Conference on Control, Instrumentation, Communication and Computational Technologies, ICCICCT 2014
Publisher	Institute of Electrical and Electronics Engineers Inc.
Pages	751-757
Number of pages	7
ISBN (Electronic)	9781479941902
DOIs	https://doi.org/10.1109/ICCICCT.2014.6993059
Publication status	Published - 01-01-2014
Event	2014 International Conference on Control, Instrumentation, Communication and Computational Technologies, ICCICCT 2014 - KanyaKumari District, Tamil Nadu, India Duration: 10-07-2014 → 11-07-2014

Conference

Conference	2014 International Conference on Control, Instrumentation, Communication and Computational Technologies, ICCICCT 2014
Country/Territory	India
City	KanyaKumari District, Tamil Nadu
Period	10-07-14 → 11-07-14

All Science Journal Classification (ASJC) codes

Computer Science(all)
Engineering(all)

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10.1109/ICCICCT.2014.6993059

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Jain, R. K., Shetty, P. K., & Shenoy, S. (2014). Experimental evaluation of PID and ESO controller for instrument landing system. In 2014 International Conference on Control, Instrumentation, Communication and Computational Technologies, ICCICCT 2014 (pp. 751-757). [6993059] Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/ICCICCT.2014.6993059

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title = "Experimental evaluation of PID and ESO controller for instrument landing system",

abstract = "This paper presents methodologies for design and experimental evaluation of both Proportional Integral and Derivative (PID) and Extended State Observer (ESO) controller for auto landing system. The process of auto landing can be experimentally described as second-order model for ES O controller. A PID controller and ES O controller is proposed to achieve the desired response for the autoland system. Computer simulations are performed to illustrate the performance of PID and ES O controller in comparison to each other. The applicability and usefulness of the proposed control scheme are well exemplified by conducting experiments on an aircraft model. Both simulations and experimental results reveal that the proposed PID and ES O scheme performs equally.",

author = "Jain, {Rahul Kumar} and Shetty, {Prashanth Kumar} and Satyanarayan Shenoy",

year = "2014",

month = jan,

day = "1",

doi = "10.1109/ICCICCT.2014.6993059",

language = "English",

pages = "751--757",

booktitle = "2014 International Conference on Control, Instrumentation, Communication and Computational Technologies, ICCICCT 2014",

publisher = "Institute of Electrical and Electronics Engineers Inc.",

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note = "2014 International Conference on Control, Instrumentation, Communication and Computational Technologies, ICCICCT 2014 ; Conference date: 10-07-2014 Through 11-07-2014",

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Jain, RK, Shetty, PK & Shenoy, S 2014, Experimental evaluation of PID and ESO controller for instrument landing system. in 2014 International Conference on Control, Instrumentation, Communication and Computational Technologies, ICCICCT 2014., 6993059, Institute of Electrical and Electronics Engineers Inc., pp. 751-757, 2014 International Conference on Control, Instrumentation, Communication and Computational Technologies, ICCICCT 2014, KanyaKumari District, Tamil Nadu, India, 10-07-14. https://doi.org/10.1109/ICCICCT.2014.6993059

Experimental evaluation of PID and ESO controller for instrument landing system. / Jain, Rahul Kumar; Shetty, Prashanth Kumar; Shenoy, Satyanarayan.

2014 International Conference on Control, Instrumentation, Communication and Computational Technologies, ICCICCT 2014. Institute of Electrical and Electronics Engineers Inc., 2014. p. 751-757 6993059.

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

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N2 - This paper presents methodologies for design and experimental evaluation of both Proportional Integral and Derivative (PID) and Extended State Observer (ESO) controller for auto landing system. The process of auto landing can be experimentally described as second-order model for ES O controller. A PID controller and ES O controller is proposed to achieve the desired response for the autoland system. Computer simulations are performed to illustrate the performance of PID and ES O controller in comparison to each other. The applicability and usefulness of the proposed control scheme are well exemplified by conducting experiments on an aircraft model. Both simulations and experimental results reveal that the proposed PID and ES O scheme performs equally.

AB - This paper presents methodologies for design and experimental evaluation of both Proportional Integral and Derivative (PID) and Extended State Observer (ESO) controller for auto landing system. The process of auto landing can be experimentally described as second-order model for ES O controller. A PID controller and ES O controller is proposed to achieve the desired response for the autoland system. Computer simulations are performed to illustrate the performance of PID and ES O controller in comparison to each other. The applicability and usefulness of the proposed control scheme are well exemplified by conducting experiments on an aircraft model. Both simulations and experimental results reveal that the proposed PID and ES O scheme performs equally.

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BT - 2014 International Conference on Control, Instrumentation, Communication and Computational Technologies, ICCICCT 2014

PB - Institute of Electrical and Electronics Engineers Inc.

T2 - 2014 International Conference on Control, Instrumentation, Communication and Computational Technologies, ICCICCT 2014

Y2 - 10 July 2014 through 11 July 2014

ER -

Experimental evaluation of PID and ESO controller for instrument landing system

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