Author : Jayanth Bhargav 1
Date of Publication :7th March 2017
Abstract: Three mode control has been traditionally used since its inception for simple and accurate control of single parameters in simple linear or piecewise linearizable systems. Aircraft cardinal angle control usually is done with more robust controllers due to the complexities and non linearities involved in their construction. But if an SISO equivalent transfer function can be derived, one can test the feasibility of PID. This paper compares the performance of traditional three mode controllers in in-loop and in-feedback configurations in order to understand the feasibility of such frameworks for autonomous flight.
Reference :
-
- Ang, K.H., Chong, G.C.Y., and Li, Y. (2005) “PID control system analysis, design, and technology”, IEEE Trans Control Systems Tech, 13(4), pp.559-576.
- Y M Zhao, “Improved Parameters tuning method for Model-Driven PID Control Systems”, IEEE Conference on Industrial Electronics and Applications (ICIEA), 2011, ISBN: 978-1-4244-8756-1
- D.V. Lukichev, G.L. Demidova, S. Brock, “Fuzzy adaptive PID control for two-mass servo-drive system with elasticity and friction,” in Proc. Cybernetics (CYBCONF), 2015, pp. 443 – 448.
- P. Derugo, K. Szabat “Implementation of the low computational cost fuzzy PID controller for two-mass drive system” in Power Electronics and Motion Control Conference and Exposition (PEMC), 2014 16th International 2014, pp. 564 – 568.
- K.J. Åström, T.H. Hägglund, "New Tuning Methods for PID controllers", Proc. 3 a European Control Conference, pp. 2456-62, 1995.
- T. Ren, T. Chen, C. Chen, "Motion control for a two-wheeled vehicle using a self-tuning PID controller", Control Engineering Practice, pp. 365-375, 2008.
- S. Jung, S.S. Kim, "Control Experiment of a WheelDriver Mobile Inverted Pendulum Using Neural Network", IEEE Transactions on Control Systems Technology, vol. 16, no. 2, pp. 297-303, 2008.