一种组合导航试验中的数据同步方法及系统

By recording the number of simulation cycles and control cycles in the satellite navigation receiver model and aligning the second pulse signal with the simulation clock signal, the problem of data misalignment caused by ground clock drift was solved, the synchronization of integrated navigation data was achieved, and the accuracy of the simulation experiment was ensured.

CN115932904BActive Publication Date: 2026-07-17BEIJING AEROSPACE AUTOMATIC CONTROL RES INST

Patent Information

Authority / Receiving Office
CN · China
Patent Type
Patents(China)
Current Assignee / Owner
BEIJING AEROSPACE AUTOMATIC CONTROL RES INST
Filing Date
2022-11-14
Publication Date
2026-07-17

AI Technical Summary

Technical Problem

In long-term ground simulation tests, ground clock drift causes mis-capture of integrated navigation data, affecting the accuracy of simulation results, which is difficult to solve effectively with existing technologies.

Method used

By recording the number of simulation cycles and control cycles in the satellite navigation receiver model, and aligning the second pulse signal and simulation clock signal, the transmission cycle of the combined navigation data is adjusted in real time to ensure the synchronization of satellite navigation receiver data and inertial measurement combined data.

Benefits of technology

During the long-term simulation, the influence of ground clock drift on the test results was eliminated, ensuring the synchronization and accuracy of the integrated navigation data, and completing the hardware-in-the-loop simulation test of the control system.

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Abstract

本发明涉及一种组合导航试验中的数据同步方法及系统。在卫星导航接收机模型计算过程中,在仿真开始后计算每个飞行控制周期时刻的接收机数据,将接收机数据区分为本控制周期数据和上一控制周期数据。根据组合导航程序在控制周期内开始计算的时间,在秒脉冲到来时刻仿真周期计数计算出秒脉冲时刻时钟漂移量,如果秒脉冲的时钟漂移量大于组合导航程序在控制周期内开始计算的时刻则本次发送本周期接收机数据,如果秒脉冲的时钟漂移量小于组合导航程序在控制周期内开始计算的时刻则发送上一控制周期的接收机数据。本发明解决在长时间仿真时,在卫星导航接收机模型计算过程中应用数据同步的问题,保证接收机数据与惯性测量组合产生的导航数据同步。
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