06.1 - Flight Dynamics and Control (Control & Modelling)
MONTE-CARLO EVALUATION OF CONTROL LAW FOR HIGH ALTITUDE FLIGHT TEST OF MARS AIRPLANE
K. Fujitaš, H. Nagaiš, H. Tokutake, Kanazawa University, Japan; A. Oyama, Institute of Space and Astronautical Science, JAXA, Japan; šInstitute of Fluid Science, Tohoku University, Japan
A Monte-Carlo simulation is performed to evaluate the success probability of the flight test of the Mars airplane at high altitude atmosphere on Earth. The number of the uncertainty parameters is 136. The simulation result shows that the success probability is 95%. It is clarified that the most severe criterion is a maximum Mach number.