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A RAPID ALIGNMENT MECHANISM APPLYING AN ADAPTIVE FILTER AND DISTURBANCE DETECTION TECHNIQUE

机译:应用自适应滤波器和扰动检测技术的快速对准机制

摘要

PURPOSE: A reliable rapid alignment mechanism for an inertial navigation system applying disturbance detection technique and an adaptive filter is provided to improve the azimuth estimation performance of the inertial navigation system. CONSTITUTION: An inertia sensor part(101) is connected to a cable. The cable outputs the output value of acceleration and an angular velocity detected by an accelerometer and a gyroscope to an approximate closed loop alignment module(102). The approximate closed-loop alignment module calculates an approximate initial posture value by using the acceleration value and an angular velocity value inputted from the inertia sensor part. A measurement shaping adaptive filter(103) uses a velocity error value induced from a posture error value or a disturbance value as a measurement value, after the approximate closed-loop alignment is completed in the approximate closed-loop alignment module. [Reference numerals] (101) Inertia sensor part; (102) Approximate closed loop alignment module; (103) Measurement shaping adaptive filter; (AA,BB) Signal
机译:目的:为惯性导航系统应用干扰检测技术和自适应滤波器提供一种可靠的快速对准机制,以提高惯性导航系统的方位角估计性能。组成:惯性传感器部件(101)已连接到电缆。电缆将由加速度计和陀螺仪检测到的加速度和角速度的输出值输出到近似闭环对准模块(102)。近似闭环对准模块通过使用从惯性传感器部输入的加速度值和角速度值来计算近似初始姿势值。在近似闭环对准模块中完成近似闭环对准之后,测量整形自适应滤波器(103)将由姿势误差值或干扰值引起的速度误差值用作测量值。 [附图标记](101)惯性传感器部分; (102)近似闭环对准模块; (103)测量整形自适应滤波器; (AA,BB)信号

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