25th Congress of International Council of the Aeronautical Sciences, 3 - 8 September 2006, Hamburg, Germany
Paper ICAS 2006-6.7.3

DESIGN OF A TRACKING CONTROL SYSTEM FOR AN OPTIMAL POST-STALL MANOEUVRE USING DYNAMIC INVERSION APPROACH

S. H. Pourtakdoust, J. Karimi, S. Shajiee
Sharif Univ. of Technology, Iran

Keywords: post stall - thrust vectoring control system [TVCS] - Herbst maneuver - dynamic inversion [DI] – optimal control

A combination of optimal and nonlinear control methodologies is utilized to perform an optimally determined trajectory as a post stall maneuver for a fighter. A closed-loop control system is designed by means of dynamic inversion. Results include of optimal state trajectories and control strategies required for tracking with/without constraints.

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