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Implementing a multi-level finite state machine with MATLAB Simulink and Stateflow in the environment of high-integrity aircraft controller software

  • Technical University of Munich

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

8 Scopus citations

Abstract

At the Technical University Munich the Institute of Flight System Dynamics uses different manned and unmanned aerial platform to demonstrate modern flight control and flight management functions. Those algorithms are designed, implemented and tested using MATLAB Simulink and Stateflow. The context of high-integrity aircraft controller software claims various limitations of the tools. The state machines used in the flight control software are developed using a special combination of MATLAB Simulink and Stateflow. That can greatly reduce complexity while simultaneously enhancing clarity and testing abilities. This paper contains a detailed explanation of the implementation scheme and structure developed at the Institute of Flight System Dynamics to design multi-level finite state machines in the context of high-integrity aircraft controller software.

Original languageEnglish
Title of host publicationProceedings - 2018 4th International Conference on Control, Automation and Robotics, ICCAR 2018
PublisherInstitute of Electrical and Electronics Engineers Inc.
Pages147-151
Number of pages5
ISBN (Electronic)9781538663387
DOIs
StatePublished - 13 Jun 2018
Event4th International Conference on Control, Automation and Robotics, ICCAR 2018 - Auckland, New Zealand
Duration: 20 Apr 201823 Apr 2018

Publication series

NameProceedings - 2018 4th International Conference on Control, Automation and Robotics, ICCAR 2018

Conference

Conference4th International Conference on Control, Automation and Robotics, ICCAR 2018
Country/TerritoryNew Zealand
CityAuckland
Period20/04/1823/04/18

Keywords

  • MATLAB
  • aircraft control
  • simulink
  • state machine
  • stateflow

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