Problems of control of mini unmanned aerial vehicle (MINIUAV)

• Autorzy: Hajduk J. , Homziuk A. , Kuliński M. , Sabak R.
• Języki publikacji: EN

Abstrakty

EN

It was introduced suggestions and results concerning some of control miniUAV problems in this article. They were formulated on base of theoretical and experimental investigations. Now the own construction miniature system avionics is being investigated. This system is designed to stabilisation of miniUAV and to control of navigation with GPS signal. Now system is used also as flight control recorder. The avionics control system which lets for very good and saved navigation miniUAV should be created. more over this system should use GPS signal and miniature sensors. Especially, a block Junction diagram of a miniature avionics unit - miniBSP MSOP. = 3 accelerometers, 3 rate gyroscopes, static pressure sensor, dynamic pressure sensor, control path in the autopilot channel of pitch and roll during the Start and Steady Flight stage, Control path in the draught control channel during Start and Steady Flight stage, general scheme of a ground-based flight control to pilot miniBSP unmanned aircrafts, visualization of the ground-based flight control station operation, airframe for testing during flight, positions of equipment items in the miniBSP airframe are presented in the paper.

Słowa kluczowe

EN

UAV; technical object; engineering; miniature avionics system

• Wydawca: Łukasiewicz Research Network - Institute of Aviation ; European Science Society of Powertrain and Transport KONES Poland ; Wydawnictwo Instytutu Technicznego Wojsk Lotniczych
• Czasopismo: Journal of KONES
• Rocznik: 2009
• Tom: Vol. 16, No. 2
• Strony: 167--173
• Opis fizyczny: rys.

Twórcy

autor

Hajduk J.

autor

Homziuk A.

autor

Kuliński M.

autor

Sabak R.

• Air Force Institute of Technology Ks. Bolesława 6 Street., 01-494 Warszawa, Poland phone: [phone],