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Micro-Electro-Mechanical-Sensor Inertial Navigation System-Assisted Global Navigation Satellite System Receiver Acquisition Scheme and Performance Evaluation 被引量:1

Micro-Electro-Mechanical-Sensor Inertial Navigation System-Assisted Global Navigation Satellite System Receiver Acquisition Scheme and Performance Evaluation
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摘要 When an aircraft moves under a low carrier-to-noise ratio (CNR) or at a high speed, increasing the sensitivity of global navigation satellite system (GNSS) receiver is a goal quite hard to achieve. A novel acquisition scheme assisted with micro-electro-mechanical-sensor (MEMS) inertial navigation system (INS) is presented to estimate the Doppler caused by user dynamics relative to each satellite ahead of time. Based on tightly coupled GNSS/INS estimation algorithm, MEMS INS Doppler error that can be achieved is first described. Then, by analyzing the mean acquisition time and signal detection probability, the MEMS INS-assisted acquisition capabilities in cold, warm and hot starts are quantitatively determined and compared with the standard GNSS acquisition capability. The simulations and comparisons have shown that: the acquisition time in cold start can be shortened by at least 23 s, the time in warm start can be shortened to i s and the acquisition capability is improved 95%, and the reaequisition time in hot start can be shortened by around 0.090 s and the capability can be enhanced 40%. The results demonstrate the validity of the novel method. When an aircraft moves under a low carrier-to-noise ratio(CNR) or at a high speed,increasing the sensitivity of global navigation satellite system(GNSS) receiver is a goal quite hard to achieve.A novel acquisition scheme assisted with micro-electro-mechanical-sensor(MEMS) inertial navigation system(INS) is presented to estimate the Doppler caused by user dynamics relative to each satellite ahead of time.Based on tightly coupled GNSS/INS estimation algorithm,MEMS INS Doppler error that can be achieved is first described.Then,by analyzing the mean acquisition time and signal detection probability,the MEMS INS-assisted acquisition capabilities in cold,warm and hot starts are quantitatively determined and compared with the standard GNSS acquisition capability.The simulations and comparisons have shown that:the acquisition time in cold start can be shortened by at least 23 s,the time in warm start can be shortened to 1 s and the acquisition capability is improved 95%,and the reacquisition time in hot start can be shortened by around 0.090 s and the capability can be enhanced 40%.The results demonstrate the validity of the novel method.
出处 《Journal of Shanghai Jiaotong university(Science)》 EI 2011年第6期728-733,共6页 上海交通大学学报(英文版)
基金 the National High Technology Research and Development Program (863) of China(No.2009AA12Z322)
关键词 global navigation satellite system (GNSS) micro-electro-mechanical-sensor (MEMS) inertial navigation system (INS) cold start warm start hot start 全球卫星导航系统 惯性导航系统 微机电传感器 采集时间 绩效评价 全球导航卫星系统 接收机 收购计划
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参考文献14

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