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 |
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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 | |
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 |
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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)