Dynamic simulation and optimization design of deployment of folding - wing 折叠翼机构展开动力学仿真及优化
The folded - wing design technique , are applied widely in the aircraft armaments , which is a most favorite scheme to solve contradictions of geometric space 折叠翼设计技术在飞行器类武器装备中具有解决几何空间矛盾的技术优势,得到了越来越多的应用。
The design principles of the folded - wing mechanisms and the working reliability need to be supported by the accurate calculation and refined analysis , so as to get to know about the work course and evaluate the effects of technical parameters 折叠翼的机械设计原理及其工作的可靠性需要细致的计算分析技术支持,获得对过程的认识并对技术参量进行定量评估。