Case studies on U-state space control system design for aircraft dynamic model

Liu, Xin; Zhu, Quanmin; Narayan, Pritesh Praneet

Abstract

In this study, U-state space design approach is used to develop a control system of linearized F-16 aircraft dynamic model. The related F-16 model is converted from the original nonlinear dynamics by Taylor series around the trimmed equilibrium. The linearized model is discretised by zero order hold. The desired closed loop matrix Ad is optimally designed by LQR (linear quadratic regulator). Then the controller output can be obtained by solve the related equations. In case study, a flight condition is selected to determine the trimmed equilibrium. The numerical simulation results show the performance of the proposed approach.

Citation

Liu, X., Zhu, Q., & Narayan, P. P. (2015, December). Case studies on U-state space control system design for aircraft dynamic model. Paper presented at 7th International Conference on Modelling, Identification and Control (ICMIC), Sousse

• Presentation Conference Type: Conference Paper (unpublished)
• Conference Name: 7th International Conference on Modelling, Identification and Control (ICMIC)
• Conference Location: Sousse
• Start Date: Dec 18, 2015
• End Date: Dec 20, 2015
• Acceptance Date: Nov 1, 2015
• Publication Date: Jan 1, 2015
• Peer Reviewed: Peer Reviewed
• Keywords: aerodynamics, aircraft control, control system synthesis, linear quadratic control, matrix algebra, state-space methods
• Public URL: https://uwe-repository.worktribe.com/output/842985
• Publisher URL: http://ipco-co.com/ICMIC/ICMIC'15.html
• Additional Information: Title of Conference or Conference Proceedings : 7th International Conference on Modelling, Identification and Control (ICMIC)