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Optimization of Fuzzy Logic Based Virtual Pilot for Wargaming

The result's identifiers

  • Result code in IS VaVaI

    <a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F60162694%3AG43__%2F21%3A00557629" target="_blank" >RIV/60162694:G43__/21:00557629 - isvavai.cz</a>

  • Result on the web

    <a href="https://www.mdpi.com/2227-7390/9/24/3169/htm" target="_blank" >https://www.mdpi.com/2227-7390/9/24/3169/htm</a>

  • DOI - Digital Object Identifier

    <a href="http://dx.doi.org/10.3390/math9243169" target="_blank" >10.3390/math9243169</a>

Alternative languages

  • Result language

    angličtina

  • Original language name

    Optimization of Fuzzy Logic Based Virtual Pilot for Wargaming

  • Original language description

    This paper deals with the design of an autopilot based on a set of fuzzy controllers. The model of the aircraft that the autopilot controls is defined as a model with 6 degrees of freedom, where the inputs to this model are the settings of the engine thrust (DX), rudder rotation (Dl) and elevators (Dm and Dn). The fuzzy controllers are of the Mamdani type, where the set of parameters defining the controller allow the derivation of membership functions of the input variables and membership functions of the output variables. The parameters of fuzzy controllers are determined by the optimization process. For the purpose of optimization, a fitness function is defined, which derives the simulation parameters from its parameter (vector), and the simulation subsequently performed and evaluated determines whether it is a feasible solution in addition the value of this solution. By this optimization process, the sub-optimal solution is found and is then used to define the settings of the fuzzy controllers and, therefore, the autopilot. This paper contains a description of each step of the solution of the described problem, and with the help of the obtained results, it is determined that the presented procedure allows us to find an autopilot capable of controlling the defined model of the aircraft. In addition, there is a brief description regarding the misconceptions explored during the development of the experiment.

  • Czech name

  • Czech description

Classification

  • Type

    J<sub>imp</sub> - Article in a specialist periodical, which is included in the Web of Science database

  • CEP classification

  • OECD FORD branch

    10101 - Pure mathematics

Result continuities

  • Project

  • Continuities

    I - Institucionalni podpora na dlouhodoby koncepcni rozvoj vyzkumne organizace

Others

  • Publication year

    2021

  • Confidentiality

    S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Data specific for result type

  • Name of the periodical

    MATHEMATICS

  • ISSN

    2227-7390

  • e-ISSN

    2227-7390

  • Volume of the periodical

    9

  • Issue of the periodical within the volume

    24

  • Country of publishing house

    CH - SWITZERLAND

  • Number of pages

    17

  • Pages from-to

    3169

  • UT code for WoS article

    000735516400001

  • EID of the result in the Scopus database

    2-s2.0-85120982545