Open AccessClassical and Modern gain estimation approach of PID controller for the pitch control of the RCTA aircraft
Author(s) -
Roli Jaiswal,
Om Prakash
Publication year - 2022
Publication title -
incas buletin
Language(s) - English
Resource type - Journals
eISSN - 2247-4528
pISSN - 2066-8201
DOI - 10.13111/2066-8201.2022.14.1.4
Subject(s) - pid controller , control theory (sociology) , controller (irrigation) , control engineering , system identification , control system , computer science , control (management) , engineering , artificial intelligence , data modeling , temperature control , agronomy , electrical engineering , database , biology
In the current age of globalization, the development of autopilots is superficial as the standard of living is improved through aerial surveillance, defense applications, and door- to-door transportation. To design the PID controller, a mathematical model is created to address the system identification for estimating longitudinal derivatives and to study the handling qualities of aircraft in order to improve piloting performance. This paper exhibits a comparative assessment between the classical closed-loop PID tuning methods like ZN, Modified ZN, Tyreus-luyben, Astrom- Hagglund and the modern control techniques like pole placement, LQR for the pitch controller design. The simulation results are displayed in the time-domain, which demonstrates the effectiveness of the approach used to design a robust controller.