@article{CAMES, author = {Zbigniew Dziopa}, title = { Rocket missile lift-off and flight simulator program}, journal = {Computer Assisted Methods in Engineering and Science}, volume = {7}, number = {4}, year = {2023}, keywords = {}, 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}, issn = {2956-5839}, pages = {507--521}, url = {https://cames.ippt.pan.pl/index.php/cames/article/view/1208} }