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Integrated Navigation System and Experiment of a Low-Cost and Low-Accuracy SINS/GPS
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作者 LIN Xueyuan XU Jin ZHOU Min 《Geo-Spatial Information Science》 2007年第3期177-180,共4页
When SINS (strap-down inertial navigation system) is combined with GPS, the observability of the course angle is weak. Although the course angle error is improved to some extent through Kalman filtering, the course ... When SINS (strap-down inertial navigation system) is combined with GPS, the observability of the course angle is weak. Although the course angle error is improved to some extent through Kalman filtering, the course angle still assumes a divergent trend. This trend is aggravated further when using low-cost and low-accuracy SINS. In order to restrain this trend, a method that uses AHRS to substitute for SINS course angle information is put forward aimed at the hardware component characteristic of the low-cost and low-accuracy SINS including AHRS (attitude and heading reference system) and IMU (inertial measurement unit), Real static and dynamic experiments show that the method can restrain the divergent trend of the navigation system angle effectively, and the positioning accuracy is high. 展开更多
关键词 low-cost and low-accuracy SINS AHRS closed-loop Kalman filter on-line adjustment
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捕获轨迹系统并联机构地面标定方法 被引量:4
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作者 谢峰 洪冠新 +2 位作者 张晨凯 魏忠武 马汉东 《航空学报》 EI CAS CSCD 北大核心 2020年第1期277-285,共9页
捕获轨迹系统(CTS)是一种先进的预测外挂物投放轨迹的试验系统,普遍采用六自由度(6-DoF)串联机构作为其运动机构,串联机构因惯性力大和关节累积误差大使其定位精准度不足。相比串联机构,并联机构具有惯性力小和关节误差不累积等优点。采... 捕获轨迹系统(CTS)是一种先进的预测外挂物投放轨迹的试验系统,普遍采用六自由度(6-DoF)串联机构作为其运动机构,串联机构因惯性力大和关节累积误差大使其定位精准度不足。相比串联机构,并联机构具有惯性力小和关节误差不累积等优点。采用6-PTRT并联机构作为CTS试验系统的六自由度运动机构,在空间受限的风洞环境中对CTS并联机构进行地面标定:提出动平台位姿的测量和计算方法,建立包含直线驱动平台安装夹角修正的标定模型,并基于非线性最小二乘法辨识结构参数。辨识后CTS并联机构的位移定位准度优于0.1mm,姿态定位准度优于0.05°,最后以CTS并联机构和常规攻角机构进行8#标模的对比风洞试验。风洞试验结果表明,CTS并联机构的风载定位准度满足测力试验精准度要求。 展开更多
关键词 捕获轨迹系统 六自由并联机构 地面标定方法 定位准度 风洞试验
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