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科技导报
|研究论文
2009
, 27
(0918) :
86
-89
特技飞行中姿态参数的测量研究
全屏
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宋双杰;张玉莲;郑泽玲
作者信息
Measurement of Posture Parameters in Aerobatics
Affiliations
出版时间: 2009-09-28
文章导航
飞机的姿态参数是研究飞机飞行状态的重要依据，在特技飞行试验中尤为重要。目前飞行试验中飞机姿态参数的测量是由全姿态组合陀螺仪完成的。在大迎角、失速、尾旋等特技飞行试验中，机载陀螺仪输出的姿态参数经数据采集系统处理后与飞机真实飞行状态之间存在误差。通过研究飞机的飞行状态与姿态参数输出特点，分析了姿态参数测量误差存在的原因，利用换向器技术改变输出多值性的问题，并在特技飞行试验中对改进的方法进行了多次验证，以期对今后大迎角、失速、尾旋等高风险、高难度特技飞行试飞中姿态参数的测量起到借鉴与指导的作用，为保证新机试飞任务顺利完成、保障飞行员生命安全提供有效的参考依据。
Attitude parameters are important among the aircraft flight parameters, especially in the aerobatic test. Current flight test aircraft attitude parameters are measured by the combination of the whole attitude gyro. In the high angle of attack, stall, spin and other special flight tests, airborne attitude gyro output parameters processed by the data acquisition system differ with the true aircraft flight conditions. By analyzing the output characteristics of the aircraft's flight status and attitude parameters, errors in the attitude parameters of measurement and the output ambiguity, this paper proposes the stunt flying test methods for improving multi-second validation, and through the analysis of the measured curves, has verified the correctness of improved methods. They may be used for future tests for large angle of attack, stall, spin high-risk, difficult aerobatic flight parameters.
aerobatics
/
profile parameters
/
measurement
/
ambiguity
宋双杰;张玉莲;郑泽玲.
特技飞行中姿态参数的测量研究.
科技导报,
2009
, 27
(0918)
: 86
-89
.
.
Measurement of Posture Parameters in Aerobatics[J].
Science & Technology Review ,
2009
, 27
(0918)
: 86
-89
.
2009年第27卷第0918期
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文章信息
接收时间：2009-05-18
首发时间：2009-09-28
出版时间：2009-09-28
收稿日期：2009-05-18
修回日期：2009-08-31
https://castjournals.cast.org.cn/joweb/kjdb/CN/1242117218822062593
引用本文
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2种不同金属材料的力学参数
科 属数 种数 占总种数比例 属 种数 占总种数比例 鹅膏菌科Amanitaceae 2 11 5.26 鹅膏菌属 Amanita 10 4.78 小菇科 Mycenaceae 2 12 5.74 丝盖伞属 Inocybe 5 2.39 多孔菌科 Polyporaceae 8 14 6.70 蜡蘑属 Laccaria 5 2.39 红菇科 Russulaceae 3 23 11.00 小皮伞属 Marasmius 6 2.87 小菇属 Mycena 11 5.26 光柄菇属 Pluteus 5 2.39 红菇属 Russula 17 8.13 栓菌属 Trametes 5 2.39
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