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准实时性前斜视INS/SAR组合导航滤波算法研究
引用本文:张旭,熊智,邵慧,刘建业.准实时性前斜视INS/SAR组合导航滤波算法研究[J].导航与控制,2012(1):1-5.
作者姓名:张旭  熊智  邵慧  刘建业
作者单位:南京航空航天大学自动化学院导航研究中心;南京航空航天大学自动化学院导航研究中心;南京航空航天大学自动化学院导航研究中心;南京航空航天大学自动化学院导航研究中心
基金项目:国家自然科学基金(编号:6090409);航空科学基金(编号:20090852012)。
摘    要:为消除常规利用正侧视SAR图像辅助导航信息对惯性误差进行修正时的滞后影响,结合前斜视SAR成像工作特性,本文分析提出了新的准实时性组合导航滤波方案和算法,以解决SAR/INS组合导航系统中的量测滞后影响;本文分析了前斜视SAR成像辅助导航系统工作特点,分析了SAR量测输出模型;建立了准实时性前斜视INS/SAR组合导航滤波算法模型,并通过仿真分析了组合导航系统性能。仿真结果表明:采用所提出的惯性/SAR组合方案和算法,可以有效克服成规正侧视SAR辅助匹配输出滞后的影响,有效满足组合系统性能要求。

关 键 词:滤波  INS/SAR组合导航  建模仿真  误差分析

Research of Quasi Real-time Squint INS/SAR Integrated Navigation Filtering Algorithm
ZHANG Xu,XIONG Zhi,SHAO Hui and LIU Jian-ye.Research of Quasi Real-time Squint INS/SAR Integrated Navigation Filtering Algorithm[J].Navigation and Control,2012(1):1-5.
Authors:ZHANG Xu  XIONG Zhi  SHAO Hui and LIU Jian-ye
Institution:Navigation research center ,Nanjing University of Aeronautics and Astronautics;Navigation research center ,Nanjing University of Aeronautics and Astronautics;Navigation research center ,Nanjing University of Aeronautics and Astronautics;Navigation research center ,Nanjing University of Aeronautics and Astronautics
Abstract:To eliminate the conventional air-borne SAR images using auxiliary information on the inertial navigation error correction lagged effect ,This paper proposed a new analysis of the quasi-real-time navigation filter programs and algorithms to solve the SAR/INS integrated navigation system the lagged effect of the measurement combined with previous squint SAR imaging features; This paper analyzes the squint SAR imaging-aided navigation system work characteristics, analysis of SAR measurement output model; established a quasi-real-time INS/SAR integrated navigation filter algorithm model, and then analysis of the integrated navigation system performance by simulation. Simulation results show that: the proposed INS / SAR combination of programs and algorithms can effectively overcome the lagging impact of the conventions SAR auxiliary navigation systems, and meet performance requirements.
Keywords:filter  INS/SAR integrated navigation system  modeling and simulation  error analysis
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