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As a basic velocity, DVL is introduced in the navigation solution process of Fiber Optic Gyro Strapdown Inertial Navigation System (FOG SINS). According to the special application background, DVL error is unavoidable to be introduced to navigation information that is calculated by FOG SINS. Firstly, the effect of DVL error on steady-state error of misalignment angles is derived. Secondly, the estimation method of DVL error is proposed: the DVL velocity error is calculated by attitude information, which is resolved respectively from compass solution method and inertial navigation solution method. At last, both simulations and ocean experiments verify the feasibility of the method. 相似文献
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A novel rapid transfer alignment algorithm for laser strapdown inertial navigation system (SINS) is studied. Transfer alignment have typically relied on velocity measurements from the master SINS as the source of alignment information, but lever arm error must be compensated accurately while velocity information is utilized, all most every quaternion based error model is nonlinear, so nonlinear filtering algorithms are need, suffering from computational complex and large error. Aim at these problems, a novel improved rapid transfer alignment algorithm formulation is presented, applying quaternion to built the process and measurement models, the improvement employs a special manipulation of the measurement equation results in a linear pseudo-measurement equation, thus the classical linear Kalman filter is employed to estimate the state, need not lever arm error compensation, results in the reduce of computational burden. Observability analysis of this new transfer alignment algorithm has been done based on the piece-wise constant system (PWCS) method, results show that the presented algorithm can accomplish the initial alignment task perfectly. A transfer alignment simulation system is also developed for the evaluation and analysis of the presented algorithm, simulation results are confirmed with the theoretical conclusion, which can achieve the transfer alignment accuracy about 1 mrad within 10 s. 相似文献
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针对现有重力导航匹配算法的匹配精度、匹配率受惯导初始位置误差影响较大以及实时性较差等不足,提出了一种基于自适应混沌蚁群径向分析的实时重力辅助导航匹配算法,新算法引入改进的连续域蚁群算法进行优化模型求解,通过进行连续域蚁群算法的信息素的自适应调整,同时对蚁群算法的搜索策略、计算参数、局部信息素进行混沌自适应处理,最终达到提高算法搜索效率、匹配率、抗噪性能的效果,实验结果表明,新算法对惯导初始误差不敏感,匹配率高,实时性强。 相似文献
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传统的地形轮廓匹配(terrain contour matching, TERCOM)算法在速度误差和航向误差较大时可靠性下降,基于扩展Kalman滤波的北航惯性地形辅助惯性导航(BUAA inertial terrain aided navigation, BITAN) 算法在初始位置误差或高度表测量噪声较大时,系统无法准确定位,导致系统的鲁棒性降低. 为解决上述问题,对BITAN算法进行改进,发展了鲁棒北航惯性地形辅助导航(robust BUAA inertial terrain aided navigation, RBITAN)算法. RBITAN算法根据平均绝对差、均方差和交叉相关算法的统计决策信息设计了搜索模式算法,以基于扩展Kalman滤波原理的BITAN算法作为跟踪算法, 综合了TERCOM算法和BITAN算法的优点,提高了算法的鲁棒性.利用真实的数字高程模型和试飞数据进行仿真验证, 并和BITAN算法进行比较.仿真结果验证了RBITAN算法可以在较大初始位置误差和较大高度表测量噪声时准确定位, 提高了算法的鲁棒性. 相似文献
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CCD接力测量船体变形研究 总被引:1,自引:1,他引:0
在舰船上,不少设备需要导航仪器提供姿态信息,船体变形会引起设备之间的姿态传递误差,导致设备效用降低。为了修正误差,获得精确的设备姿态测量结果,需要一套测量装置对船体变形进行测量。基于CCD的船体变形测量具有非接触性、精度高的优点。但当测量的两设备安装基座之间光路不能通视时,需要采用接力测量方法。阐述了CCD接力测量船体变形方法的原理和模型,并进行了模拟试验。试验结果表明,CCD接力测量船体变形方法可以高精度测量设备之间的相对姿态变化量。 相似文献
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应用MEMS陀螺仪测量人体手臂运动姿态时,针对陀螺仪受线加速度干扰导致测量姿态发散的问题,提出基于Kalman滤波算法的姿态误差补偿方法;该方法首先将陀螺仪采集到的角速度通过方向余弦算法解算得到姿态角,并将陀螺仪动态漂移造成的姿态角误差视为时变信号,通过建立姿态角漂移误差的状态方程及观测方程,应用卡尔曼滤波算法,实现对姿态角漂移误差的估计,最终达到对陀螺仪动态漂移误差的补偿;实验与仿真结果表明,应用该算法能够有效的抑制线加速度干扰导致的陀螺仪测量的姿态发散,适用于陀螺仪对人体手臂运动姿态的测量。 相似文献
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根据单矢量水听器自身具有阵列流型的特点,提出了适用于对目标保持连续跟踪的空域预滤波MUSIC算法。通过调整滤波器通带中心角使其保持在目标估计方位角附近,可以消除滤波器通带中心角偏离目标真实方位角时传统预滤波MUSIC算法产生的目标方位估计误差。仿真结果表明,改进预滤波MUSIC算法可以减小甚至消除低信噪比情况下目标方位估计存在的较大误差。海试数据结果表明,阵元域MUSIC和改进预滤波MUSIC都可实现对单频脉冲信号和线性调频信号的目标方位估计,且估计结果与GPS舰位推算结果一致,但改进预滤波MUSIC算法主瓣更尖锐。对宽带航船噪声处理结果显示,改进预滤波MUSIC算法使单矢量水听器在存在目标干扰时的探测距离从2 km提升到了5 km,验证了改进预滤波MUSIC算法可实现弱目标情况下的高分辨目标方位跟踪。 相似文献
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为了实现低成本SINS初始对准,降低对准过程复杂程度,提高系统对准精度,缩短对准时间,本文引入了EMD滤波技术。首先,采集IMU输出信号,根据EMD算法将信号分解为IMF簇,按照CMSE标准对信号进行重构,完成信号滤波处理;接着,按照AR模型对经EMD滤波前后的数据噪声进行建模;然后,分别利用原始信号和EMD降噪后信号进行SINS姿态粗对准;最后,根据IMU模型和SINS误差模型,采用零速对准方式,完成SINS精对准。实验结果表明:经EMD降噪后的信号粗对准精度为1.3°,精对准精度为0.87 mrad,精对准收敛时间为200 s。 相似文献
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AR模型辅助SINS/GPS组合导航的实验研究 总被引:1,自引:1,他引:0
激光陀螺的随机漂移噪声类似于白噪声,可以采用AR(2)模型进行数字滤波来减小其对激光陀螺精度的影响。首先介绍了AR模型,然后利用IMU单元三组陀螺信号的AR(2)模型给出了车载SINS/GPS组合导航系统误差模型,并在GPS的辅助下,对SINS/GPS组合导航进行了实验研究。最后利用Kalman滤波器对车载SINs/GPS组合导航实际测量数据进行了离线的半实物仿真。实验结果表明,采用AR(2)模型辅助的SINS/GPS组合导航系统能够得到较高的姿态精度,并能有效抑制速度误差的发散。 相似文献
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单个矢量水听器直方图算法具有良好的鲁棒性和目标方位估计性能,该文对直方图算法目标探测性能进行了分析和总结,并提出了一种基于目标方位估计的水中目标自主探测与跟踪算法,该算法可实现水中目标有无自主检测。仿真和消声水池测试结果表明,直方图算法实现目标自主跟踪所要求的信噪比需大于-7 dB,此时测向误差约为8°,-3 dB方位谱宽度在20°左右。海上试验数据分析表明,直方图算法对航速8.4 kn的水面航船在距离13.8 km范围内,可实现全程目标探测和跟踪,测向误差最优可达5?,在距离2 km时-3 dB方位谱宽度可达10°左右。 相似文献
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Marine propulsion unit (MPU) is one of the dominant vibration and noise sources onboard ship. Its vibration can be attenuated effectively by isolating MPU with low-frequency mounting system. But this is difficult to implement due to the stringent requirement of MPU alignment with the propulsion shafting. In this paper a novel air spring mounting system (ASMS) for propulsion system is proposed consisting of air spring subsystem, alignment control subsystem and safety protection subsystem. The load distribution optimization method and dynamic model of ASMS are presented. The factors that affect system stability and natural frequencies are analyzed, as well as the design measures to enhance system performance. A theoretical model is presented to estimate the isolation effect of ASMS. The monitoring model of alignment between MPU and propulsion shafting is established, followed by the alignment control algorithm and converge rule which assures the fast and uniform convergence of both air springs? load distribution and alignment control process. Safety protection mechanism is designed to ensure that the MPU can operate safely in case of ASMS failure or other extreme circumstances. A scaled ASMS prototype is manufactured and tested on a special experimental setup. Experimental results validate the effectiveness of theoretical models and show that the performance of ASMS satisfies the operation requirements of MPU. 相似文献
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针对传统船摇隔离度测试方法效率低、误差大、操作复杂、且不能有效解决扰动跳变的不足,对船摇隔离的基本原理进行了分析,建立了梯度型最小二乘滤波模型,提出了基于梯度型最小二乘滤波和VC++语言编程实现船摇隔离度的自动测试方法,并利用跟踪实测数据进行了仿真实验。对比传统方法测试结果表明,该方法能有效滤除测量数据中的随机误差,较大程度地降低了扰动跳变的抖动量,提高了伺服系统船摇隔离度的测试精度。 相似文献