@inproceedings{ce5a26910bd04ca3a6acca28782da059,
title = "Monte-Carlo evaluation of control law for high altitude flight test of Mars airplane",
abstract = "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.",
keywords = "Control, Flight simulation, Flight test, Monte-Carlo simulation, UAV",
author = "Koji Fujita and Hiroki Nagai and Hiroshi Tokutake and Akira Oyama",
note = "Publisher Copyright: {\textcopyright} 31st Congress of the International Council of the Aeronautical Sciences, ICAS 2018. All rights reserved.; 31st Congress of the International Council of the Aeronautical Sciences, ICAS 2018 ; Conference date: 09-09-2018 Through 14-09-2018",
year = "2018",
language = "English",
series = "31st Congress of the International Council of the Aeronautical Sciences, ICAS 2018",
publisher = "International Council of the Aeronautical Sciences",
booktitle = "31st Congress of the International Council of the Aeronautical Sciences, ICAS 2018",
}