06.1 - Flight Dynamics and Control (Control & Modelling)
EVALUATION OF ALTITUDE CONTROL FOR AN AIRBREATHING HYPERSONIC AIRCRAFT MODEL
M. Hiruma, The University of Tokyo, Japan
The objective of the research presented in this paper is to simulate and design the rocket launch/aircraft separation condition as well as the flight trajectory for the Hypersonic Experimental Aircraft to achieve the engine test conditions by applying PID control from air data gained from Flush Air Data System (FADS).