A Simple Optimization Method for Tuning the Gains of PID Controllers for the Autopilot of Cessna 182 Aircraft Using Model-in-the-Loop Platform

Author:

Freire Fernando Palmieri,Martins Nardênio AlmeidaORCID,Splendor Fábio

Publisher

Springer Science and Business Media LLC

Subject

Electrical and Electronic Engineering,Computer Science Applications,Energy Engineering and Power Technology,Control and Systems Engineering

Reference19 articles.

1. Blakelock, J. H. (1991). Automatic control of aircraft and missiles. New York: Wiley.

2. Cook, M. V. (2007). Flight dynamics principles. A linear systems approach to aircraft stability and control (2nd ed.). Oxford: Butterworth-Heinemann.

3. do Carmo, M. J., Oliveira, Â. R., & Carvalho, J. R. (2012). Use of statistics as non-intrusive indexes in the evaluation of behavior of the control loops: A case study for systems with transport delay. In XXXVI national congress of applied and computational mathematics (CNMAC) (vol. 2194, pp. 1034–1040). (in Portuguese).

4. Franklin, G. F., Powell, J. D., & Emami-Naeini, A. (2015). Feedback control of dynamic systems (7th edition, Global Edition). New York: Pearson.

5. Kada, B., & Ghazzawi, Y. (2011). Robust pid controller design for an UAV flight control system. Lecture Notes in Engineering and Computer Science, 2194, 945–950.

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