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直升机悬停及低速飞行阶段轴间耦合试飞技术
引用本文:宋庆国.直升机悬停及低速飞行阶段轴间耦合试飞技术[J].飞行力学,2004,22(3):69-72.
作者姓名:宋庆国
作者单位:中国飞行试验研究院,试飞员学院,陕西,西安,710089
摘    要:从试飞员角度出发,分析了直升机轴间耦合现象产生的原因,讨论了ADS-33D规范中有关轴间耦合问题的要求,提出了武装直升机轴间耦合试飞方法、数据处理方法、试飞驾驶技术要点以及试验过程中应注意的事项,可供从事武装直升机飞行试验的技术人员和试飞员参考。

关 键 词:悬停及低速飞行阶段  轴间耦合  试飞技术
文章编号:1002-0853(2004)03-0069-04
修稿时间:2003年7月31日

Research on Flight Test Technique for the Armed Helicopter Inter-Axis Coupling during Hover & Low Speed Phases
SONG Qing-guo.Research on Flight Test Technique for the Armed Helicopter Inter-Axis Coupling during Hover & Low Speed Phases[J].Flight Dynamics,2004,22(3):69-72.
Authors:SONG Qing-guo
Abstract:As viewed from a test pilot, the cause for the inter-axis coupling phenomenon of a helicopter is analyzed. Some requirements about the inter-axis problem in ADS-33D are discussed. According to the flight test program, flight-test pilot's skills and data processing methods of the inter-axis flight test for the armed helicopter are given out. Also some matters needing the attention during the flight test are mentioned. It provides a reference to technicians and test pilots engaging in armed helicopter flight tests.
Keywords:hovering & low speed flight phases  inter-axis  coupling  flight test technique
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