摘要
本文介绍了机动飞行中俯仰动态反应的三个判别准则,并通过J-7飞机的试飞,测量和计算了这些判据,以便比较和验证这三个准则的适用性。同时在试飞中,采用精确控制姿态法,开展了驾驶员的定量评价研究,进一步验证了这三个准则.
In this paper, three specifications of pitch dynamic response in maneuvering flying are presented. In flying test of a J-7 aircraft, these judged criterions were measured and computed, so that these specifications are compared and proofed according to their suitability. In addition, used a method of precise control of pitch attitude in the flight test, quantitative pilot ratings search was developed, so that the three specifications are proofed further.
出处
《飞行力学》
CSCD
北大核心
1990年第3期51-59,共9页
Flight Dynamics
