view Abstract and Download![]() shooting. This paper presents a 3 degrees of freedom dynamic system simulation of the launching device system using MATLAB. The�relationship between thrust of the rocket and vibration characteristics�of the rocket-launching device system is an important portion in�order to analyze and design for more stable and precise launching�mechanism. The result of understudied dynamic system simulation�of a 3 degrees of freedom of rocket-launching device reveals that�thrust of the rocket is significantly correlated with the vibration of launching device system. The data from the simulation result can be�used lately for the structural design improvement, the firing azimuth�and elevation angle adjustment, sequence of firing, and period of�rocket firing. A 3 Degrees of Freedom Dynamic System.pdfLogin Required |
ติดตามผ่านสื่อ Social ที่ : Facebook, Youtube
เว็บไซต์สถาบันเทคโนโลยีสารสนเทศ ขออนุญาตใช้คุ๊กกี้เพื่อให้เว็บไซต์ทำงานได้เต็มประสิทธิภาพ ท่านสามารถอ่านนโยบายคุ้กกี้ได้ ที่นี่.