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Modelling of the UAV safety manoeuvre for the air insertion operations

The result's identifiers

  • Result code in IS VaVaI

    <a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F60162694%3AG42__%2F16%3A00532672" target="_blank" >RIV/60162694:G42__/16:00532672 - isvavai.cz</a>

  • Alternative codes found

    RIV/61989100:27200/16:86098826

  • Result on the web

    <a href="http://vavtest.unob.cz/registr" target="_blank" >http://vavtest.unob.cz/registr</a>

  • DOI - Digital Object Identifier

    <a href="http://dx.doi.org/10.1007/978-3-319-47605-6_27" target="_blank" >10.1007/978-3-319-47605-6_27</a>

Alternative languages

  • Result language

    angličtina

  • Original language name

    Modelling of the UAV safety manoeuvre for the air insertion operations

  • Original language description

    Tempo and complexity of the contemporary asymmetric battlefield is on the increase and time for a certain component delivery (ammunition, medical kit, vaccine and so on), for instance in the special operations, could be critical. Usually, the only way in these situations is a fast air delivery of concrete material to the „hot“ destination zone. Contemporary air insertion in that case is usually performed by manned or unmanned (if available) system with human intuitive manoeuvre planning supported by information from ISR systems. In this case, there is almost impossible to achieve a fast, detailed and mathematically optimal solution with the real time implementation to the UAV control system (autopilot). The article describes a modelling approach which leads to high automation and optimal (autonomous) reasoning in case of 3D UAV path planning, respecting the operational situation in the area, manoeuvre limits of the UAV and potential threat in the operational area. The solution is based on detailed operational area 3D modelling, known and unknown probabilistic threat simulation and its capa-bility estimation, quantification of safety area parameters and large 3D (multi-criteria) safety matrix development, criterial function and boundary condition specification, UAV air manoeuvre and constraints algorithm development, opti-mal UAV path search and operational evaluation.

  • Czech name

  • Czech description

Classification

  • Type

    D - Article in proceedings

  • CEP classification

    KA - Militarism

  • OECD FORD branch

Result continuities

  • Project

  • Continuities

    I - Institucionalni podpora na dlouhodoby koncepcni rozvoj vyzkumne organizace

Others

  • Publication year

    2016

  • Confidentiality

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

Data specific for result type

  • Article name in the collection

    Modelling and Simulation for Autonomous Systems, MESAS 2016

  • ISBN

    978-3-319-47604-9

  • ISSN

    0302-9743

  • e-ISSN

  • Number of pages

    10

  • Pages from-to

    337-346

  • Publisher name

    Springer International Publishing

  • Place of publication

    Rome

  • Event location

    Rome

  • Event date

    Jun 15, 2016

  • Type of event by nationality

    WRD - Celosvětová akce

  • UT code for WoS article

    000389939300027