34th Congress of the International Council of the Aeronautical Sciences

06.1 - Flight Dynamics and Control (Control & Modelling)

EXPLICIT MODEL FOLLOWING TRAJECTORY CONTROL SYSTEM FOR MULTIPLE VERTICAL TAKEOFF AND LANDING CONFIGURATIONS

A. Comer¹, I. Chakraborty¹; ¹Auburn University, United States

This paper demonstrates a flight control system architecture suitable for Simplified Vehicle Operations and applicable to three dissimilar vehicle configurations. It utilizes a novel Trajectory Control System for controlling longitudinal dynamics coupled to explicit model following inner-loop control. This is demonstrated through representative maneuver simulations.


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