这个程序演示了如何应用耦合结构空气动力问题，通过Matlab编程，分析了飞行器机翼颤振等问题。-This model demonstrates how to implement a coupled structural-aerodynamic problem. The wing, otherwise rigid, is allowed to pitch and plunge. The motion of the wing is defined using SimMechanics bloc

按正弦方式变化的攻角控制规律，利用MATLAB对HTV-2跳跃滑翔式飞行器弹道过程进行了仿真-Tracking the development plans of The DARPA/AF Falcon program，the program calculates the reentry skipping trajectory