首页|基于锁相环的高旋飞行体滚转角估计方法

基于锁相环的高旋飞行体滚转角估计方法

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针对高旋飞行体滚转角速率难以直接测量的问题,通过分析高旋飞行体的角运动特征,建立了滚转角运动模型,提出了一种基于地磁信息和锁相跟踪的滚转角估计方法.首先利用最小二乘过零检测方法,提取地磁传感器测量的角频率信息,进而解算得到高旋飞行体的转速信息,再根据高旋飞行体角运动特性和俯仰、偏航轴陀螺测量信号特性确定三阶锁相环环路滤波参数,对提取的角频率信息和转速信息进行锁频锁相跟踪.通过软件仿真和载体试验分别对滚转角估计方法进行了验证.结果表明:利用三阶锁相环方法对高旋飞行体滚转角频率进行有效跟踪,能够获取滚转角速度和滚转角,满足高旋飞行体姿态实时解算要求.
Roll Angle Estimation Method of High-rotation Flying Body Based on Phase-locked Loop
In order to accurately measure the roll angle of the high-spinning flying body,a roll angle motion model was established by analyzing the motion characteristics,and a roll angle estimation method based on geomagnetic information and phase-locked tracking was proposed.First,the angular frequency information measured by geomagnetic sensor was extracted by least square zero-crossing detection method,and the rotational speed information of high spinning flying body was solved.Then,the filter parameters of the third-order phase-locked loop were determined according to the angular motion characteristics of high spinning flying body and the measured signals of pitch and yaw axis gyroscopes,and the extracted angular frequency information and rotational speed information were tracked by frequency-locked phase-locked tracking.The roll angle estimation method was verified by the simulation and test.The results show that the third-order phase-locked loop method is utilized to effectively track the roll angular frequency of the high-spinning flying body,and the roll angular velocity and roll angle can be obtained to meet the requirements of real-time attitude solution of the high-spinning flying body.

high spinning flying bodythird-order phase-locked looproll angle frequencyroll attitudetest validation

王桂奇、刘福朝、李存健

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北京信息科技大学自动化学院

北京信息科技大学高动态导航技术北京市重点实验室

高旋飞行体 三阶锁相环 滚转角频率 滚转姿态 试验验证

北京市自然科学基金项目北京市教委科技一般项目高动态导航技术北京市重点实验室资助

4212003KM202311232015

2024

仪表技术与传感器
沈阳仪表科学研究院

仪表技术与传感器

CSTPCD北大核心
影响因子:0.585
ISSN:1002-1841
年,卷(期):2024.(6)
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