Monte-Carlo evaluation of control law for high altitude flight test of Mars airplane

Koji Fujita, Hiroki Nagai, Hiroshi Tokutake, Akira Oyama

Research output: Chapter in Book/Report/Conference proceedingConference contribution

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.

Original languageEnglish
Title of host publication31st Congress of the International Council of the Aeronautical Sciences, ICAS 2018
PublisherInternational Council of the Aeronautical Sciences
ISBN (Electronic)9783932182884
Publication statusPublished - 2018 Jan 1
Event31st Congress of the International Council of the Aeronautical Sciences, ICAS 2018 - Belo Horizonte, Brazil
Duration: 2018 Sep 92018 Sep 14

Publication series

Name31st Congress of the International Council of the Aeronautical Sciences, ICAS 2018

Other

Other31st Congress of the International Council of the Aeronautical Sciences, ICAS 2018
CountryBrazil
CityBelo Horizonte
Period18/9/918/9/14

Keywords

  • Control
  • Flight simulation
  • Flight test
  • Monte-Carlo simulation
  • UAV

ASJC Scopus subject areas

  • Electrical and Electronic Engineering
  • Control and Systems Engineering
  • Materials Science(all)
  • Aerospace Engineering

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