Adaptive fading Kalman filter algorithm for RTK (Real-Time Kinematic) technology

A filtering algorithm and self-adaptive technology, applied in radio wave measurement systems, satellite radio beacon positioning systems, measurement devices, etc., can solve the problems of difficult to accurately establish filter system models, poor filter robustness, and divergence.

Active Publication Date: 2018-06-29
BEIJING AUTOMATION CONTROL EQUIP INST
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Problems solved by technology

However, when the Kalman filter is used for real-time dynamic differential positioning, the motion state of the maneuvering carrier is complex and changeable, and the system model of the filter is difficult to establish accurately. Due to the poor robustness of the standard Kalman filter, it is easy to cause divergence
At present, the first-order time correla

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  • Adaptive fading Kalman filter algorithm for RTK (Real-Time Kinematic) technology
  • Adaptive fading Kalman filter algorithm for RTK (Real-Time Kinematic) technology
  • Adaptive fading Kalman filter algorithm for RTK (Real-Time Kinematic) technology

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Embodiment Construction

[0081] The technical solutions of the present invention will be described in detail below in conjunction with specific embodiments.

[0082] 1. a kind of RTK uses self-adaptive fading Kalman filtering algorithm, is characterized in that, comprises the steps: (1) satellite captures tracking and synchronization

[0083] The base station and the rover capture satellite navigation signals sequentially, and perform bit synchronization and frame synchronization on the tracking satellites;

[0084] (2) Observation extraction

[0085] The satellite observations after frame synchronization are extracted, and the ephemeris parameters of each navigation satellite after frame synchronization are obtained; the satellite observations after frame synchronization include satellite pseudorange and carrier phase observations.

[0086] (3) Determine the satellite position and speed calculation

[0087] Input the ephemeris parameters obtained in the known satellite launch time and step (2) to c...

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Abstract

The invention belongs to the field of satellite navigation differential receivers, and relates to a design algorithm capable of improving the dynamic adaptability solved by an ambiguity floating solution by using an adaptive fading Kalman filter. According to an adaptive fading Kalman filter algorithm, a single-difference cycle ambiguity is added into a state vector of a filter model for filter estimation, and a forgetting factor is introduced to improve the dynamic tracking performance of the filter. In addition, an independent sliding window is introduced for collection and processing of innovation, so that the problem that an innovation covariance cannot be accurately calculated due to observed quantity interruption caused by a reference star change or loss of lock of a satellite signalis solved. The algorithm is easy to apply, and no complicated equations or equations with huge calculation volumes are needed; arithmetic programming can be realized on a DSP (Digital Signal Processor) or FPGA (Field Programmable Gate Array) hardware platform according the aspects of the instantaneity and the calculation volume, namely engineering implementation is facilitated.

Description

technical field [0001] The invention belongs to the field of satellite navigation differential receiver design, and relates to a design algorithm for solving dynamic adaptability of a floating-point solution of ambiguity by using an adaptive fading Kalman filter. Background technique [0002] Carrier phase-based dynamic differential technology (RTK technology) is a high-precision positioning technology, which has a wide range of applications, such as high-precision navigation guidance, UAV approach and landing, and so on. The key of RTK technology is the fast and accurate solution of the ambiguity of the whole circle. Among them, the most widely used ambiguity resolution algorithm is the LAMBDA algorithm, which is divided into two processes: ambiguity real number estimation and ambiguity integer search. The real estimate of the ambiguity provides an initial search value for the ambiguity parameter, usually a floating point number. The high-precision ambiguity floating-poin...

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Application Information

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IPC IPC(8): G01S19/44
CPCG01S19/44
Inventor 高亚豪左启耀李峰胡文涛袁晓宇王强王勋李建华邹志勤姜福灏
Owner BEIJING AUTOMATION CONTROL EQUIP INST
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