Integrated navigation – flight control system of guided projectiles and bombs

• Autorzy: Vogt R. , Adamski M. , Głębocki R.

Identyfikatory

DOI

10.15632/jtam-pl.53.1.119

• Języki publikacji: EN

Abstrakty

EN

Integrated navigation and flight control systems have found a widespread use in projectiles. Currently, due to their advantages, they begin to be used more frequently in airplanes and helicopters. The paper presents one of the most advanced solutions of the integrated navigation – the flight control system designed for guidance of projectiles and aerial bombs.

Słowa kluczowe

EN

navigation; flight control system; bomb

• Wydawca: Polskie Towarzystwo Mechaniki Teoretycznej i Stosowanej
• Czasopismo: Journal of Theoretical and Applied Mechanics
• Rocznik: 2015
• Tom: Vol. 53 nr 1
• Strony: 119--123
• Opis fizyczny: Bibliogr. 5 poz., rys.

Twórcy

autor

Vogt R.

• Polish Air Force Academy, Faculty of Aviation and Aeronautics, Dęblin, Poland

autor

Adamski M.

• Polish Air Force Academy, Faculty of Aviation and Aeronautics, Dęblin, Poland

autor

Głębocki R.

• Warsaw University of Technology, Faculty of Power and Aeronautical Engineering, Warsaw, Poland

Bibliografia

• 1. Głębocki R., Vogt R., 2000, Impulse control of anti-tank missile, NATO-RTO Meeting Proceeding, Brunschwig
• 2. Głębocki R., Vogt R., 2007, Guidance systems of smart mortar missile, The Archive of Mechanical Engineering, LIV, 1
• 3. Grzesik N., 2011, Zaawansowane systemy uzbrojenia lotniczego. Budowa i zastosowanie, WSOSP, Dęblin
• 4. Koruba Z., Ładyżyńska-Kozdraś E., 2010, The dynamic model of combat target homing system of the unmanned aerial vehicle, Journal of Theoretical and Applied Mechanics, 48, 3, 551-566
• 5. Stefański K., Koruba Z., 2012, Analysis of the guiding of bombs an ground targets using a gyroscope system, Journal of Theoretical and Applied Mechanics, 50, 4, 473-485