Further, the determination method of target service life is provided for general maneuver flight load conbined with spin flight load. 本文进一步介绍了在机动飞行和螺旋载荷掺合作用下目标寿命的确定方法。
A general mathematical method with subsection function is given to describe helicopter maneuver, most of mission task elements ( MTE ) defined in ADS-33E-PRF can be modeled. 本文提出了一个较通用的直升机机动科目分段函数描述方法,该方法可以对ADS-33E-PRF规定的大部分任务科目建立逆仿真所需的数学模型。