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2020 27th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS)最新文献

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Classification of Map-Aided Navigation Algorithms 地图辅助导航算法的分类
Pub Date : 2020-05-01 DOI: 10.23919/icins43215.2020.9133757
Oleg A. Stepanov, A. Nosov, A. Toropov
A map-aided navigation problem is formulated in the Bayesian framework to provide a basis for algorithms classification. Algorithms involving preprocessing of measurements aimed to improve the accuracy of the field profile used in the comparison with the map are discussed. An algorithm without measurements preprocessing and profile estimation is briefly described. The results are considered to illustrate the operation and advantages of such an algorithm by an example of a gravity-aided navigation in a weakly anomalous region.
在贝叶斯框架中提出了一个地图辅助导航问题,为算法分类提供了依据。讨论了在与地图比较中用于提高野外剖面精度的测量预处理算法。简要介绍了一种不进行测量预处理和轮廓估计的算法。最后以弱异常区域重力辅助导航为例,说明了该算法的有效性和优越性。
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引用次数: 2
Application of Kalman Type Filtering for Processing Navigation Data With Nonlinear Dynamics and Measurements 卡尔曼滤波在非线性动力学和测量导航数据处理中的应用
Pub Date : 2020-05-01 DOI: 10.23919/icins43215.2020.9133846
V. A. Tupysev, Y. Litvinenko, A. Isaev
The paper discusses the possibility of increasing the efficiency of the Kalman type filters for nonlinearities in the dynamics and measurement equations by using a special finite-difference equation to choose the linearization point. The simulation results of navigation data processing problem illustrate the effectiveness of the proposed approach
本文讨论了用一种特殊的有限差分方程选择线性化点来提高卡尔曼滤波器处理动力学方程和测量方程非线性的效率的可能性。导航数据处理问题的仿真结果表明了该方法的有效性
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引用次数: 2
Improving the Quality of the Transient Process of the Compensation Pendulum Accelerometer with LMI control 用LMI控制改善补偿摆加速度计瞬态过程的质量
Pub Date : 2020-05-01 DOI: 10.23919/icins43215.2020.9133864
V. Nikiforov, M. Tchaikovsky, A. Gusev, K. Andreev, A.S. Anokhin, N.P. Stikhareva
This article discusses the synthesis of a static regulator based on LMI-control with varying the correction coefficient. The mathematical modeling of the proposed regulator was carried out. Conclusions about the application of the proposed method are drawn.
本文讨论了一种基于可变修正系数lmi控制的静态调节器的合成。对所提出的调节器进行了数学建模。最后对该方法的应用进行了总结。
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引用次数: 3
Investigation of Nonlinear High-Intensity Dynamic Processes in a Non-ideal Solid-State Wave Gyroscope Resonator 非理想固体波陀螺谐振腔中非线性高强度动态过程的研究
Pub Date : 2020-05-01 DOI: 10.23919/icins43215.2020.9133943
M. Basarab, B. Lunin, D. Vakhlyarskiy, E. Chumankin
A numerical-analytical method for solving the dynamic equation of an elastic ring resonator mounted on an arbitrarily rotating base is proposed. The method is based on the combined use of the generalized Bubnov-Galerkin (Kantorovich) method in angle and the direct method (Rothe) in time variable. In contrast to the previously presented results, the initial model takes into account terms proportional to the square of the angular velocity of the base and angular acceleration; it is also assumed that the resonator parameters are not uniform in angle. The given example allows us to conclude that the method is suitable for the case of high-intensity dynamic processes (large square of angular velocity and angular acceleration), in particular, the effect of reducing the influence of the defect of the resonator parameters by the 4th harmonic on its dynamics is shown.
提出了一种求解任意旋转基座上弹性环形谐振器动力学方程的数值解析方法。该方法结合了广义Bubnov-Galerkin (Kantorovich)方法和直接法(Rothe)方法在时间变量上的应用。与先前提出的结果相反,初始模型考虑了与基底角速度和角加速度的平方成正比的项;同时假定谐振腔参数在角度上不均匀。给出的算例表明,该方法适用于高强度动态过程(角速度和角加速度的大平方)的情况,特别是显示了用四次谐波减少谐振器参数缺陷对其动力学的影响。
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引用次数: 3
Research on Rotation Scheme of Hybrid Inertial Navigation System with Three Rotating Axes 三旋转轴混合惯性导航系统旋转方案研究
Pub Date : 2020-05-01 DOI: 10.23919/icins43215.2020.9133768
B. Guan, S. Li, Q. Fu
Hybrid inertial navigation system with three rotating axes involves the advantages of platform navigation system, strapdown navigation system and rotatory inertial navigation systems, which can improve navigation and positioning accuracy substantially. A comprehensive study of the error propagation properties and error compensation mechanism of rotatory inertial navigation system is conducted. On the basis of this theory, combined with the analysis of the traditional rotation scheme, a reasonable scheme of system error compensation based on the geographical coordinate system is determined. The rotation scheme relative to the geographic frame cannot eliminate the coupling items between the errors of the gyroscope and the Earth rotation, then a three-axis rotation scheme relative to inertial frame is proposed. The simulation is conducted to verify the rotation scheme, and the results are compared with the rotation scheme relative to the geographical frame. Results show that the inertial frame modulation scheme can reduce the navigation error caused by coupling items between the errors of the gyroscope and the Earth rotation obviously.
三旋转轴混合惯性导航系统综合了平台式导航系统、捷联式导航系统和旋转式惯性导航系统的优点,可以大幅度提高导航定位精度。对旋转惯导系统的误差传播特性和误差补偿机制进行了全面的研究。在此理论的基础上,结合对传统旋转方案的分析,确定了基于地理坐标系的系统误差补偿的合理方案。相对于地理坐标系的旋转方案不能消除陀螺仪与地球自转误差之间的耦合项,因此提出了相对于惯性坐标系的三轴旋转方案。通过仿真验证了旋转方案,并将结果与相对于地理框架的旋转方案进行了比较。结果表明,惯性系调制方案能明显减小由于陀螺仪误差与地球自转之间的耦合项所引起的导航误差。
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引用次数: 2
A Review on ZUPT-Aided Pedestrian Inertial Navigation zupt辅助行人惯性导航研究进展
Pub Date : 2020-05-01 DOI: 10.23919/icins43215.2020.9133730
Yusheng Wang, A. Shkel
We present a review of studies that were conducted by the MicroSystems Laboratory at UC Irvine on ZUPT-aided pedestrian inertial navigation. Our most recent results include: adaptive ZUPT detection, IMU mounting position optimization, residual velocity characterization, IMU error calibration, and navigation error prediction. With all the efforts above, a robust and accurate ZUPT-aided pedestrian inertial navigation implementation was demonstrated. The navigation bias was reduced by 10×, and a position error of less than 1% of the total length of trajectory was demonstrated with an industrial-grade IMU.
我们提出了由加州大学欧文分校微系统实验室进行的关于zupt辅助行人惯性导航的研究综述。我们最近的研究成果包括:自适应ZUPT检测、IMU安装位置优化、剩余速度表征、IMU误差校准和导航误差预测。在此基础上,提出了一种鲁棒、精确的zupt辅助行人惯性导航实现方案。在工业级IMU上,导航偏差减小了10倍,位置误差小于弹道总长度的1%。
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引用次数: 9
A Novel Magnetometer Calibration Approach with Artificial Data 一种新的人工数据磁强计校准方法
Pub Date : 2020-05-01 DOI: 10.23919/icins43215.2020.9133787
Nhan Nguyen, P. Müller
This paper proposes two methods for calibrating triaxial magnetometers. Both of them calibrate these sensors with more general assumption of noise on three axes than previous state-of-the-art methods. The first method estimates bias and rotation parameters more accurately and the second method yields a better estimate for the scaling parameter than the state-of-the-art method subMLE. The computational time of the latter is also 43 times faster than subMLE, which allows this method to be applied in devices with low-computational resources (e.g. smartphones). Furthermore, the second method yields more robust heading angle estimates compared to subMLE. This result implies that the second method can be applied in light-weight inertial measurement systems, for which the orientation of the device is vital information for pedestrian dead reckoning system.
本文提出了三轴磁强计的两种标定方法。他们都校准这些传感器与更一般的假设噪声在三个轴上比以前的最先进的方法。第一种方法对偏置和旋转参数的估计更准确,第二种方法对尺度参数的估计比最先进的subMLE方法更好。后者的计算时间也比subMLE快43倍,这使得该方法可以应用于计算资源较少的设备(例如智能手机)。此外,与subMLE相比,第二种方法产生了更稳健的航向角估计。该结果表明,第二种方法可以应用于轻型惯性测量系统,其中装置的方向是行人航位推算系统的重要信息。
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引用次数: 1
Development of Methods for Identification of Nonlinear Mathematical Model Parameters of Solid-State Wave Gyroscope 固态波陀螺仪非线性数学模型参数辨识方法的发展
Pub Date : 2020-05-01 DOI: 10.23919/icins43215.2020.9133967
A. Maslov, D. A. Maslov, I. Merkuryev, V. V. Podalkov
Identification of parameters of a solid-state wave gyroscope in the forced and free-run modes under nonlinear resonator oscillation is considered. By using the Krylov-Bogolyubov averaging method, calibration equations are deduced for determining the mathematical model coefficients. These coefficients contain an oscillation nonlinearity coefficient and parameters characterizing resonator defects including frequency difference and damping anisotropy, orientation of main axes of stiffness and dissipation. Suggested identification methods allow us to perform testing at large oscillation amplitudes. Numerical simulation of parameters identification is carried out. It is shown that accounting for nonlinearities in case of large oscillation amplitudes significantly increases the accuracy of parameters identification.
研究了非线性谐振腔振荡下固体波陀螺仪在强迫和自由运行模式下的参数辨识问题。采用Krylov-Bogolyubov平均法,推导了确定数学模型系数的标定方程。这些系数包含振荡非线性系数和表征谐振器缺陷的参数,包括频率差和阻尼各向异性、主轴刚度方向和耗散。建议的识别方法允许我们在大振荡幅度下进行测试。对参数辨识过程进行了数值模拟。结果表明,在振荡幅度较大的情况下,考虑非线性可以显著提高参数辨识的精度。
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引用次数: 1
Promising Aircraft Navigation Systems with Use of Physical Fields: Stationary Magnetic Field Gradient, Gravity Gradient, Alternating Magnetic Field 利用物理场的有前途的飞机导航系统:静止磁场梯度,重力梯度,交变磁场
Pub Date : 2020-05-01 DOI: 10.23919/icins43215.2020.9133854
E. Karshakov, B. Pavlov, I. Papusha, M. Tkhorenko
The report presents the analysis of opportunities of aircraft navigation systems development with regard to the aid of onboard geophysical fields measurements. We consider some prospective systems which today are not widely used: magnetic gradiometers that measure stationary magnetic field gradient, gravity gradiometers that measure gravity field gradient, electromagnetic systems that measure the alternating part of magnetic field. We discuss the main tasks that have to be solved during airborne measurements of these parameters. We give a review of algorithms and hardware solutions. We present some examples of onboard measurements and estimate the possible navigation accuracy.
该报告分析了借助机载地球物理场测量技术发展飞机导航系统的机会。我们考虑了一些目前尚未广泛应用的有前景的系统:测量静止磁场梯度的磁梯度仪,测量重力场梯度的重力梯度仪,测量磁场交变部分的电磁系统。讨论了在这些参数的机载测量中必须解决的主要问题。我们给出了算法和硬件解决方案的回顾。我们给出了一些机载测量的例子,并估计了可能的导航精度。
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引用次数: 3
Using Broadcast Corrections for Calculating GNSS-GNSS Time Offset 利用广播校正计算GNSS-GNSS时间偏移
Pub Date : 2020-05-01 DOI: 10.23919/icins43215.2020.9133797
P. Bogdanov, A. Druzhin, T. Primakina
To provide positioning and timing in multisystem mode by signals from Space Vehicles (SV) of different Global Navigation Satellite Systems (GNSS) it is necessary to provide users with the values of the offsets between GNSS time scales. The paper is aimed at comparing different methods of calculating GNSS-GNSS Time offsets by the users for multisystem mode.
为了利用不同全球导航卫星系统(GNSS)的空间飞行器(SV)信号提供多系统模式下的定位授时,需要向用户提供GNSS时标间的偏移值。本文旨在比较用户在多系统模式下计算GNSS-GNSS时间偏移的不同方法。
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2020 27th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS)
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