摘要
姿态敏捷性是反映武装直升机机动能力的一项重要指标。通过对中等幅度下的姿态敏捷性的试飞原理的分析,得到其与操纵功效之间的区别。对于不同的响应类型,给出了对应的试飞操纵输入方法。最后,依据ADS-33E对某型武装直升机的仿真数据进行了分析。
Attitude quickness is an important parameter that reflects the maneuverability of aimedhelicopter. By analyzing the theory of flight test technology for moderate-amplitude attitudequickness, the differences from control power are gained. For the different response types, it offersthe different test control methods. At last, the simulation data of armed helicopter is analyzedaccording to ADS-33E.
出处
《工程与试验》
2017年第4期6-9,共4页
Engineering and Test
