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飞机迎角在垂直阵风干扰中的卡尔曼滤波估计
引用本文:赵元峰,唐永哲,赵宝庆.飞机迎角在垂直阵风干扰中的卡尔曼滤波估计[J].飞行力学,2006,24(3):53-55,60.
作者姓名:赵元峰  唐永哲  赵宝庆
作者单位:西北工业大学,自动化学院,陕西,西安,710072
摘    要:在阵风条件下,为了抑制飞机的附加载荷并改善乘坐品质,需要得到飞机的迎角状态。以某大型运输机为例,通过卡尔曼滤波方法,将飞机法向过载和俯仰角速度综合进飞机的操纵输入来估计垂直阵风条件下的飞机迎角,并进行了仿真。结果表明,在垂直阵风干扰条件下,采用卡尔曼滤波方法能获得迎角状态的良好估计。

关 键 词:迎角  垂直阵风  卡尔曼滤波估计
文章编号:1002-0853(2006)03-0053-03
收稿时间:2005-07-05
修稿时间:2005-07-052006-06-15

Angle of Attack's Kalman Filter Estimation in Vertical Gust
ZHAO Yuan-feng,TANG Yong-zhe,ZHAO Bao-qing.Angle of Attack''''s Kalman Filter Estimation in Vertical Gust[J].Flight Dynamics,2006,24(3):53-55,60.
Authors:ZHAO Yuan-feng  TANG Yong-zhe  ZHAO Bao-qing
Abstract:In the condition of gust,in order to restrain additional load and improve the comfort of passenger,the state of angle of attack is acquired.By additional angle of attack vertical gust influences the movement of a transport,and causes normal load and pitch rate response.By Kalman filter,in conditions of vertical gust the angle of attack is estimated.An example is given and simulated.The results demonstrate Kalman filter has a good performance,and the estimated angle-of-attack well accords with its actual state.
Keywords:angle of attack  vertical gust  Kalman filter estimation  
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