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The pseudolite-based indoor navigation system using Ambiguity Resolution On The Fly

机译:基于歧义解析的基于伪卫星的室内导航系统

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This paper presents a method of AROF (Ambiguity Resolution On The Fly) with extended Kalman filter (EKF) to resolve ambiguities for pseudolite-based indoor navigation system. The carrier phase measurements of pseudolites can obtain high positioning precision. In many pseudolite systems which recently have been proposed and tested, pseudolites are usually used to offer positioning and navigation applications in indoor or blocked environments. However, like indoor environment, the carrier phase measurements of pseudolite are not entirely same as GPS. A major difference is carrier phase integer ambiguity resolution. The traditional way of ambiguity resolution (AR) for GPS is static or kinematic initialization. But the static initialization is not suitable for pseudolites. Using pseudolites for static initialization, the equations are correlated with each other at observation epochs and the ambiguities can't be calculated from the equations. As a result, the integer ambiguity resolution is using the initial position of receiver as a known parameter. This paper proposes a method of ambiguity resolution on the fly (AROF) with EKF, which doesn't need to know the staring vector of receiver and achieve the kinematic initialization of carrier phase measurement in pseudolite-based indoor navigation system. As same as GPS measurement equations, Dual-Differential observation model is given based on indoor-pseudolite positioning system, which is non-linear and dynamic model. In general, the standard Kalman filter can't deal with this nonlinear situation, since the covariance equations are based on the linearized system and not the true nonlinear system. So, the best approach to this problem is to use the Extended Kalman Filter (EKF). As a result of this approach, the measurement equations of the Kalman filter become linear, and the computational requirements are significantly reduced, making it possible to estimate ambiguity in real time. Extensive testing of the filter with s--ynthetic data proved it to be satisfactory. Test cases included the presence of large initial errors as well as high noise levels. In all cases the filter was able to get ambiguities.
机译:本文提出了一种带有扩展卡尔曼滤波器(EKF)的AROF(飞行歧义解决方案)方法,以解决基于伪卫星的室内导航系统的歧义。伪卫星的载波相位测量可以获得很高的定位精度。在最近已经提出和测试的许多伪卫星系统中,伪卫星通常用于在室内或封闭环境中提供定位和导航应用。但是,像室内环境一样,伪卫星的载波相位测量与GPS并不完全相同。主要区别在于载波相位整数歧义分辨率。 GPS的歧义分辨率(AR)的传统方法是静态或运动学初始化。但是静态初始化不适用于伪卫星。使用伪卫星进行静态初始化时,这些方程在观测时期相互关联,并且无法从这些方程计算出模棱两可。结果,整数歧义分辨率将接收器的初始位置用作已知参数。提出了一种基于EKF的动态模糊度解算(AROF)方法,该方法不需要知道接收机的凝视矢量,就可以在基于伪卫星的室内导航系统中实现载波相位测量的运动学初始化。与GPS测量方程一样,基于室内伪卫星定位系统给出了双微分观测模型,它是非线性的动态模型。通常,标准卡尔曼滤波器无法处理这种非线性情况,因为协方差方程基于线性化系统,而不是真正的非线性系统。因此,解决此问题的最佳方法是使用扩展卡尔曼滤波器(EKF)。这种方法的结果是,卡尔曼滤波器的测量方程变为线性,并且显着降低了计算要求,从而可以实时估计歧义。使用s-对过滤器进行广泛的测试 -- 综合数据证明它是令人满意的。测试案例包括较大的初始错误以及较高的噪声水平。在所有情况下,过滤器都能够消除歧义。

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