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Micro PNT system based on GNSS, chip atomic clock and micro inertial navigation

A chip atomic clock, micro-inertial navigation technology, applied in the radio wave measurement system, satellite radio beacon positioning system, navigation and other directions, can solve the problems of self-error accumulation, self-correction, inertial navigation system can not work for a long time, etc., to achieve The effect of low cost, convenient improvement and update, and fast calculation speed

Inactive Publication Date: 2017-09-26
NANJING UNIV OF SCI & TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The inertial navigation system is based on Newton's classical laws of mechanics. It uses accelerometers and gyroscopes to determine the position, velocity and attitude of the carrier through coordinate transformation and integral algorithms. By transmitting or receiving signals, the positioning and navigation functions can be completed through its own system, which has excellent autonomy and concealment, but its own errors will accumulate over time and cannot be corrected by itself. This fatal shortcoming makes independent The inertial navigation system cannot work for a long time

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  • Micro PNT system based on GNSS, chip atomic clock and micro inertial navigation
  • Micro PNT system based on GNSS, chip atomic clock and micro inertial navigation
  • Micro PNT system based on GNSS, chip atomic clock and micro inertial navigation

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Embodiment 1

[0061] combine figure 1 , the micro-PNT system of the present invention, the system is based on the micro-architecture of DSP+FPGA+CASC+MIMU, including a GNSS navigation module, a chip atomic clock module, and a micro-inertial navigation module: the GNSS navigation module receives GNSS signals in the sky and obtains navigation measurement values and navigation message, use the navigation measurement value and navigation message to perform positioning calculation, and finally obtain the user's satellite information and obtain the positioning observation value; the chip atomic clock module can provide accurate 1pps second pulse and precise 10MHz crystal oscillator signal, after taming, it can Independently provide accurate 1pps second pulse for use by the navigation processor to realize independent timing function; the micro-inertial navigation module sends the angular rate measured by the gyroscope and the specific force output by the accelerometer to the data processing unit th...

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Abstract

The invention discloses a micro PNT system based on GNSS, chip atomic clock and micro inertial navigation. The system is based on DSP, FPGA, chip atomic clock and micro inertial navigation, and comprises a radio frequency front-end processing module, a baseband signal digital processing module, a micro inertial navigation module, a chip atomic clock module and a data processing module, wherein the radio frequency front-end processing module is used for performing amplification, frequency conversion, filtering and analog-digital conversion on satellite signals to obtain digital intermediate frequency signals; the baseband signal digital processing module processes the digital intermediate frequency signals to obtain navigation measuring values and navigation messages; the micro inertial navigation module performs calculation by a navigation algorithm to obtain navigation information; after being trained, the chip atomic clock module independently provides 1pps (pulse per second) for the data processing module to be used; the data processing module performs positioning calculation by using the navigation measuring values and the navigation messages, performs combined navigation by using satellite navigation data and inertial navigation data, and outputs position, speed, accelerated speed, posture and time information. The micro PNT system is applicable to high dynamic range, has small long-term drift and has the advantages of low cost, small size, low power consumption, light weight and plug and play effect.

Description

technical field [0001] The invention relates to the technical field of positioning, navigation and timing microsystems, in particular to a micro-PNT system based on GNSS, chip atomic clock and micro-inertial navigation. Background technique [0002] With the continuous development of society, people's demand for location and time information is becoming more and more intense. At present, the global satellite navigation system is gradually improving and improving. With many advantages such as convenience and unlimited number of users, it is the most cost-effective positioning, navigation and timing system. However, due to the physical characteristics of satellite navigation signals, their vulnerability is determined. In complex electromagnetic environments such as physically obstructed environments, electronic countermeasures, and spectrum countermeasures, the service performance will be severely degraded, or even fail to work. [0003] Therefore, the satellite navigation in...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01C21/16G01C21/20G01S19/47
CPCG01C21/165G01C21/20G01S19/47
Inventor 陈帅孙昭行卢启伟赵琛汪益平陈德潘张嘉瑞姚晓涵赵志鑫
Owner NANJING UNIV OF SCI & TECH
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