Evolutionary algorithms in stabilization of unmanned aerial vehicles

Result code in IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F70883521%3A28140%2F08%3A63507783" target="_blank" >RIV/70883521:28140/08:63507783 - isvavai.cz</a>

Result on the web

—

DOI - Digital Object Identifier

—

Result language

čeština

Original language name

Evoluční algoritmy při stabilizaci bezpilotních prostředků (UAV)

Original language description

The article discusses the calculation of intervention into the aircraft controls for model/unmanned aerial vehicle (UAV) trim under different flight situations and configurations using the global optimization theory and computer simulation. The artificial intelligence methods and heuristic algorithms dealing with the system of nonlinear differential equations of motion in a multidimensional space of potential solutions are presented here. The main aim was to find the steady-state flight characteristicslocating the stable minima of a proposed cost function. The new approach is presented here with employment of self-organizing migrating algorithm and differential evolution for finding the optimal solution. the method shown here may be practically utilized as for the aircraft design as well as the UAV control.

Czech name

Evoluční algoritmy při stabilizaci bezpilotních prostředků (UAV)

Czech description

The article discusses the calculation of intervention into the aircraft controls for model/unmanned aerial vehicle (UAV) trim under different flight situations and configurations using the global optimization theory and computer simulation. The artificial intelligence methods and heuristic algorithms dealing with the system of nonlinear differential equations of motion in a multidimensional space of potential solutions are presented here. The main aim was to find the steady-state flight characteristicslocating the stable minima of a proposed cost function. The new approach is presented here with employment of self-organizing migrating algorithm and differential evolution for finding the optimal solution. the method shown here may be practically utilized as for the aircraft design as well as the UAV control.

Type

D - Article in proceedings

CEP classification

BC - Theory and management systems

OECD FORD branch

—

Project

<a href="/en/project/GA102%2F06%2F1132" target="_blank" >GA102/06/1132: Softcomputing in Control</a><br>

Continuities

P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)

Publication year

2008

Confidentiality

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

Article name in the collection

Civilní bezpilotní systémy 2008

ISBN

978-80-902522-2-6

ISSN

—

e-ISSN

—

Number of pages

27

Pages from-to

—

Publisher name

Odborná společnost letecká České republiky

Place of publication

Praha

Event location

Praha

Event date

Nov 13, 2008

Type of event by nationality

CST - Celostátní akce

UT code for WoS article

—