Rocket missile lift-off flight simulator program

• Autorzy: Dziopa Z.
• Konferencja: Polish Conference on Computer methods in mechanics ; (14 ; 26-28.05.1999 ; Rzeszów, Poland
• Języki publikacji: EN

Abstrakty

EN

The subject of this paper is a movable antiaircraft short-range rocket set. The control algorithm for a target homing short-range rocket missile by means of the proportional approach method is performed by an executive system comprising the co-ordinator and automatic pilot devices. The co-ordinator is equipped with a gyro-device and a system determining working out of the ideal, desirable signal. The automatic pilot device has a pair of double-position external vanes and internal gas control engine. A missile control, in accordance with the implemented algorithm, is achieved by using a rocket rotating motion around its longitudinal axis.

Słowa kluczowe

EN

rocket missile; flight simulator program

PL

pocisk rakietowy; program symulujący lot

• Wydawca: Instytut Podstawowych Problemów Techniki PAN
• Czasopismo: Computer Assisted Mechanics and Engineering Sciences
• Rocznik: 2000
• Tom: Vol. 7, No. 4
• Strony: 507--521
• Opis fizyczny: Bibliogr. 6 poz., rys

Twórcy

autor

Dziopa Z.

• Technical University of Kielce [Poltechnika Świętokrzyska], al. Tysiąclecia Państwa Polskiego 7, 25-314 Kielce, Poland

Bibliografia

• [1] S. Dubiel. Generalised constraints and their application in flying objects controlability. WAT Bulletin supplement, Warsaw, 1973.
• [2] Z. Dziopa. Influence of launcher—rocket missile system arrangement on rocket missile flight phase. WAT Bulletin, 69-78, Warsaw, 1996.
• [3] Z. Dziopa. Compilation of the mathematical model of longitudinal axis of rotating short-range missile rocket lift-off and flight. Research and Development Centre of Skarżysko, 297, Skarżysko-Kamienna, 1997.
• [4] Z. Dziopa. Controlling the longitudinal axis rotating short-range missile rocket. Scientific Brochures of Rzeszów Engineering College, Avionics, 125-132. Rzeszów, 1998.
• [5] M. Glapski. Possibilities and limitations of air-to-air missiles proportional homing. WAT Bulletin supplement, Warsaw, 1985.
• [6] J. Nisiol. Gyro dynamics with particular regard to the integrating gyro in neces-sitarian and probabilistic nonlinear expression. Cracow Technical University, Cracow, 1975.