Modelling of the UAV safety manoeuvre for the air insertion operations
Identifikátory výsledku
Kód výsledku v 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>
Nalezeny alternativní kódy
RIV/61989100:27200/16:86098826
Výsledek na webu
<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>
Alternativní jazyky
Jazyk výsledku
angličtina
Název v původním jazyce
Modelling of the UAV safety manoeuvre for the air insertion operations
Popis výsledku v původním jazyce
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.
Název v anglickém jazyce
Modelling of the UAV safety manoeuvre for the air insertion operations
Popis výsledku anglicky
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.
Klasifikace
Druh
D - Stať ve sborníku
CEP obor
KA - Vojenství
OECD FORD obor
—
Návaznosti výsledku
Projekt
—
Návaznosti
I - Institucionalni podpora na dlouhodoby koncepcni rozvoj vyzkumne organizace
Ostatní
Rok uplatnění
2016
Kód důvěrnosti údajů
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů
Údaje specifické pro druh výsledku
Název statě ve sborníku
Modelling and Simulation for Autonomous Systems, MESAS 2016
ISBN
978-3-319-47604-9
ISSN
0302-9743
e-ISSN
—
Počet stran výsledku
10
Strana od-do
337-346
Název nakladatele
Springer International Publishing
Místo vydání
Rome
Místo konání akce
Rome
Datum konání akce
15. 6. 2016
Typ akce podle státní příslušnosti
WRD - Celosvětová akce
Kód UT WoS článku
000389939300027