sapiСистемный анализ и прикладная информатика«System analysis and applied information science»2309-49232414-0481Belarusian National Technical Universitysapi-22Research ArticleУправление техническими объектамиManagement of technical objectsУПРАВЛЕНИЕ ТРАЕКТОРИЕЙ ПОЛЕТА БЕСПИЛОТНОГО ЛЕТАТЕЛЬНОГО АППАРАТАFLIGHT PATH CONTROL FOR UNMANNED AERIAL VEHICLEАль-МашхаданиМ. А.Al-MashhadaniM. A.

Аспирант

CA_PI@bntu.byБелорусский национальный технический университетБеларусьBelarusian National Technical UniversityBelarus20140705201401-33840Copyright © Аль-Машхадани М., 20142014Аль-Машхадани М.Al-Mashhadani M.Данная работа распространяется под лицензией Creative Commons Attribution 4.0.This work is licensed under a Creative Commons Attribution 4.0 License.https://sapi.bntu.by/jour/article/view/22

Проведено исследование оптимизированного по заданному критерию закона управления беспилотного летательного аппарата при наведении его по траектории, заданной опорными точками в инерциальной системе координат. Приводится пример, иллюстрирующий работоспособность предложенных теоретических положений.

Studying the optimized control law specified criteria on UAV while hovering over a path defined by the reference points in the inertial frame. An illustrative example is the  theoretical efficiency of the proposed provisions.

 

ReferencesLavalle S. M. Rapidly-exploring random trees: A new tool for path planning/Computer Science Department, Iowa State University, 1998.Lavalle S. M. Rapidly-exploring random trees: A new tool for path planning/Computer Science Department, Iowa State University, 1998.Anderson E. P. An Algorithmic Implementation of Constrained External Control for UAVs/ E. P. Anderson, R. W. Beard // AIAA Guidance, Navigation, and Control Conference and Exhibit, Monterey, Canada, 2002. P. 4470.Anderson E. P. An Algorithmic Implementation of Constrained External Control for UAVs/ E. P. Anderson, R. W. Beard // AIAA Guidance, Navigation, and Control Conference and Exhibit, Monterey, Canada, 2002. P. 4470.Lobaty А. А. Analytical synthesis control for unmanned aerial vehicle / А. А. Lobaty, А. А. Antanovich, Y. F. Ikuas // Collection of articles, Belarus – 2009. – № 17. – P. 62–66.Lobaty А. А. Analytical synthesis control for unmanned aerial vehicle / А. А. Lobaty, А. А. Antanovich, Y. F. Ikuas // Collection of articles, Belarus – 2009. – № 17. – P. 62–66.Control and guidance of unmanned aircraft maneuvering on the basis of modern information technologies /Edited by М. N. Krasilschikov and G. G. Serebriakov. Phys-math.– М.: 2005. P. 280.Control and guidance of unmanned aircraft maneuvering on the basis of modern information technologies /Edited by М. N. Krasilschikov and G. G. Serebriakov. Phys-math.– М.: 2005. P. 280.Merkolov, V. E. Aircraft radio system. Vol.2. Electronic systems homing / Edited by. А. E. Каnashinkov and V. E. Меrkolov. – М.: radiotechnics, 2003. P. 390.Merkolov, V. E. Aircraft radio system. Vol.2. Electronic systems homing / Edited by. А. E. Каnashinkov and V. E. Меrkolov. – М.: radiotechnics, 2003. P. 390.Bryson А. Applied optimal control theory / А. Bryson, Ho Yu-shi. – М.: World, 1972. P. 544.Bryson А. Applied optimal control theory / А. Bryson, Ho Yu-shi. – М.: World, 1972. P. 544.Handbook of control theory / Edited by. А. А. Krasowski. – М.: science. Chief Editor phys.-маth., 1987. P. 712.Handbook of control theory / Edited by. А. А. Krasowski. – М.: science. Chief Editor phys.-маth., 1987. P. 712.

The authors declare that there are no conflicts of interest present.