中国惯性技术学报
中國慣性技術學報
중국관성기술학보
JOURNAL OF CHINESE INERTIAL TECHNOLOGY
2013年
6期
775-780
,共6页
闫捷%徐晓苏%张涛%刘义亭%吴亮
閆捷%徐曉囌%張濤%劉義亭%吳亮
염첩%서효소%장도%류의정%오량
组合导航%捷联惯性导航%全球定位系统%导航计算机%卡尔曼滤波
組閤導航%捷聯慣性導航%全毬定位繫統%導航計算機%卡爾曼濾波
조합도항%첩련관성도항%전구정위계통%도항계산궤%잡이만려파
integrated navigation%SINS%GNSS%navigation computer%Kalman filter
针对舰载小型化导航设备功耗低、体积小、可靠性好、精度高的性能需求,研制出基于嵌入式DSP与FPGA架构的SINS/GNSS舰载小型化组合导航系统平台。首先,在系统硬件方面,阐述了系统的总体设计方案,构建了嵌入式导航计算机平台,介绍了系统所采用的光纤陀螺、石英挠性加速度计和 GNSS 接收机的性能指标。其次,在导航算法方面,介绍了舰载小型化 SINS/GNSS 紧组合导航系统的工作原理,分析了捷联惯性导航系统和 GNSS 的噪声误差模型,设计了基于 SINS/GNSS 的紧组合工作模式下的扩展卡尔曼滤波器。最后,进行了样机车载验证实验。实验结果表明:该组合导航系统水平姿态误差小于0.02°(1σ),航向误差小于0.1°(1σ),水平位置定位误差小于2 m(1σ),能够满足舰载小型化导航设备的低功耗、高可靠性、高精度等需求。
針對艦載小型化導航設備功耗低、體積小、可靠性好、精度高的性能需求,研製齣基于嵌入式DSP與FPGA架構的SINS/GNSS艦載小型化組閤導航繫統平檯。首先,在繫統硬件方麵,闡述瞭繫統的總體設計方案,構建瞭嵌入式導航計算機平檯,介紹瞭繫統所採用的光纖陀螺、石英撓性加速度計和 GNSS 接收機的性能指標。其次,在導航算法方麵,介紹瞭艦載小型化 SINS/GNSS 緊組閤導航繫統的工作原理,分析瞭捷聯慣性導航繫統和 GNSS 的譟聲誤差模型,設計瞭基于 SINS/GNSS 的緊組閤工作模式下的擴展卡爾曼濾波器。最後,進行瞭樣機車載驗證實驗。實驗結果錶明:該組閤導航繫統水平姿態誤差小于0.02°(1σ),航嚮誤差小于0.1°(1σ),水平位置定位誤差小于2 m(1σ),能夠滿足艦載小型化導航設備的低功耗、高可靠性、高精度等需求。
침대함재소형화도항설비공모저、체적소、가고성호、정도고적성능수구,연제출기우감입식DSP여FPGA가구적SINS/GNSS함재소형화조합도항계통평태。수선,재계통경건방면,천술료계통적총체설계방안,구건료감입식도항계산궤평태,개소료계통소채용적광섬타라、석영뇨성가속도계화 GNSS 접수궤적성능지표。기차,재도항산법방면,개소료함재소형화 SINS/GNSS 긴조합도항계통적공작원리,분석료첩련관성도항계통화 GNSS 적조성오차모형,설계료기우 SINS/GNSS 적긴조합공작모식하적확전잡이만려파기。최후,진행료양궤차재험증실험。실험결과표명:해조합도항계통수평자태오차소우0.02°(1σ),항향오차소우0.1°(1σ),수평위치정위오차소우2 m(1σ),능구만족함재소형화도항설비적저공모、고가고성、고정도등수구。
In order to meet the performance requirements of low power consumption, small size, high reliability and high accuracy of the marine navigation equipment, an embedded DSP and FPGA structure-based marine SINS/GNSS integrated navigation system was studied and designed. Firstly, in terms of hardware, the system general hardware was expounded. The performance index of FOG, quartz flexible accelerometer and GNSS receiver which were used in the system was introduced. Secondly, in terms of navigation algorithm, the working principle of marine-based SINS/GNSS integrated navigation system was introduced, and the error model of inertial navigation system and GNSS was analyzed. The extended Kalman filter in the SINS/GNSS tight combination mode was designed. Finally, the experiment of prototype vehicle verification was made. The results of vehicle experiment show that the horizontal attitude error of the integrated navigation system is less than 0.02°(1σ), the heading error is less than 0.1°(1σ) and the positioning error is less than 2 m(1σ), which meet the marine-based equipment’s navigational requirements such as low power consumption, high reliability and high precision.