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A Synthetic Aperture Radar Inertial Navigation Data Input Method and Input Agent System

A technology of synthetic aperture radar and input method, which is applied in the field of inertial navigation data input agent system to achieve the effects of low coupling degree, improved reliability and reduced clock source

Active Publication Date: 2018-04-06
CHINA ELECTRONIC TECH GRP CORP NO 38 RES INST
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

The standard serial port module usually uses sixteen times the clock of the serial port baud rate, and it is only used by the serial port

Method used

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  • A Synthetic Aperture Radar Inertial Navigation Data Input Method and Input Agent System
  • A Synthetic Aperture Radar Inertial Navigation Data Input Method and Input Agent System

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Embodiment Construction

[0032] A kind of agent-based synthetic aperture radar inertial navigation data input method and inertial navigation data input proxy system of the present invention will be further described below in conjunction with accompanying drawings and specific embodiments:

[0033] The present invention is an agent-based synthetic aperture radar inertial navigation data input method and inertial navigation data input agent system, which are used to obtain inertial navigation data from inertial navigation equipment and provide complete data to DSP by designing agents in FPGA frame.

[0034] Such as figure 1 As shown, the inertial navigation data input agent system used in the agent-based synthetic aperture radar inertial navigation data input method includes a serial port monitoring serial-to-parallel conversion module 1, an adaptive framing module 2, an agent management module 3, and a signal processing RAM interface module 4. The serial port monitoring serial-to-parallel conversion m...

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Abstract

The invention discloses an agent-based synthetic aperture radar inertial navigation data input method and an inertial navigation data input agent module. The method comprises the following steps: using an input status of inertial navigation data, an operation behavior and status of a DSP port, conflict monitoring and management at a read end and a write end of an application-level inertial navigation data cache as objects monitored and managed by an agent by adopting the agent-based technology, monitoring serial data and performing framing processing on the serial data according to an inertial navigation frame, adopting a status driving manner in the frame processing procedure, automatically monitoring the behavior of the DSP port and providing the inertial navigation data to a DSP according to a complete frame protocol on the basis of the status of the DSP port. The inertial navigation data input agent module comprises a serial port monitoring serial-parallel conversion module, a self-adaptive framing module, an agent management module and a signal processing RAM interface module. Through the adoption of the method and the agent module disclosed by the invention, the efficiency is high, the system coupling degree is low, and the operation is simpler, and the possibility of data clogging can be reduced, the differential processing is realized, the number of the clock sources is reduced, and the reliability is improved.

Description

Technical field: [0001] The invention relates to an agent-based synthetic aperture radar inertial navigation data input method and an inertial navigation data input agent system, which uses an agent-based design instead of a high-performance processor to complete receiving inertial navigation data to form an application-level frame protocol, so that the signal processor Focus on handling high-performance computing. Background technique: [0002] SAR (Synthetic Aperture Radar) is a high-resolution imaging radar that forms a virtual equivalent long antenna through the movement of the radar on the flight carrier to obtain radar images with high azimuth resolution. The synthesis of the effective long antenna by the linear motion of the aircraft is the principle of forming the synthetic aperture, which is also the problem of the synthetic aperture radar. During the flight, the motion error of the aircraft will lead to problems such as unstable beam pointing and non-uniform sampl...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G06F13/38
Inventor 夏际金赵洪立钮俊清崔留争习建博潘浩王杰潘勇先朱鹏
Owner CHINA ELECTRONIC TECH GRP CORP NO 38 RES INST