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- Title
Classical and Modern gain estimation approach of PID controller for the pitch control of the RCTA aircraft.
- Authors
JAISWAL, Roli; PRAKASH, Om
- Abstract
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.
- Subjects
POLE assignment; MODEL airplanes; AERIAL surveillance; SYSTEM identification; STANDARD of living; PID controllers
- Publication
INCAS Bulletin, 2022, Vol 14, Issue 1, p39
- ISSN
2066-8201
- Publication type
Article
- DOI
10.13111/2066-8201.2022.14.1.4