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Control algorithm relative attitude of unmanned aerial vehicles

Keywords:

V.P. Kharkov - Ph.D. (Eng.), Professor, Chief Research Scientist, JSC «E\'ksperimental\'naya masterskaya Nauka Soft» (Moscow). E-mail: charkovvp@rambler.ru


Safe formation of a system of UAV of a complex configuration and safe control of it is offered for executing with use of an element of a formation which is understood as group of UAV consisting from 2, n = 0,1,2,3,… airplanes. Control synthesis is executed with use of a method of return problems of dynamics. The fulfilled modeling has shown efficiency of controls, its suitability for control as pair of UAV, and any elements of a formation.
References:

 

  1. Ostoslavskijj I.V., Strazheva I.V. Dinamika poleta. Ustojjchivost i upravljaemost letatelnykh apparatov. M.: Mashinostroenie. 1965.
  2. Bjushgens G.S., Studnev R.V. Aehrodinamika samoleta, Dinamika prodolnogo i bokovogo dvizhenija. M.: Mashinostroenie. 1979.
  3. KHarkov V.P. Adaptivnoe upravlenie dinamicheskimi sistemami na osnove obratnykh zadach dinamiki // Izv. ANSSSR. Tekhnicheskaja kibernetika. 1994. № 4. S. 115–124.

 

June 24, 2020
May 29, 2020

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