Rocket missile lift-off and flight simulator program
Abstract
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
References
[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.
[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.
Published
2023-03-29
Issue
pp. 507-521
Section
Articles
License
Copyright © The Author(s).
This work is licensed under the Creative Commons Attribution 4.0 International CC BY 4.0.
How to Cite
Dziopa, Z. (2023). Rocket missile lift-off and flight simulator program. Computer Assisted Methods in Engineering and Science, 7(4), 507-521. https://cames3.ippt.pan.pl/index.php/cames/article/view/1208
