Adaptive filtering of tracking camera data and onboard sensors for a small helicopter autopilot

A. Barabanov, D. Romaev
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引用次数: 5

Abstract

A navigation system was designed for an autopilot of a small helicopter. It contains two remote web cameras and an onboard sensor with three gyroscopes and three accelerometers. The camera positions are unknown. The gyroscope and accelerometer measurements have unknown random bias with a slow trend. For estimation of these parameters an adaptive filtering system with the extended Kalman filter is developed. Tuning of the filter parameters is made online by minimization of the high frequency part of the helicopter velocity estimate. A new method is also developed for smoothing of the big oscillations forced by rotation of the main rotor that appear in the gyroscope measurements of the angular velocity. The method is based on equations from the helicopter motion model that give a relation between linear accelerations and the Euler angles estimated by integration of the angular velocity measurements.
小型直升机自动驾驶仪跟踪相机数据和机载传感器的自适应滤波
设计了一种用于小型直升机自动驾驶仪的导航系统。它包含两个远程网络摄像头和一个带有三个陀螺仪和三个加速度计的机载传感器。摄像机的位置是未知的。陀螺仪和加速度计的测量结果具有未知的随机偏差和缓慢的趋势。为了估计这些参数,提出了一种扩展卡尔曼滤波的自适应滤波系统。通过最小化直升机速度估计的高频部分,实现滤波器参数的在线整定。本文还提出了一种新的方法来平滑陀螺仪测量角速度时出现的主转子旋转引起的大振荡。该方法基于直升机运动模型的方程,该方程给出了线加速度与欧拉角之间的关系,该关系由角速度测量值的积分计算得到。
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