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1.
A CE-5T1 spacecraft completed a high-speed skip re-entry to the earth after a circumlunar flight on October 31, 2014. In addition to the strapdown inertial navigation system (SINS), a lightweight GPS receiver with rapid acquisition was developed as a navigation sensor in the re-entry capsule. The GPS receiver effectively solved the poor accuracy problem of long-term navigation using only the SINS. In contrast to ground users and low-earth-orbit spacecraft, numerous factors, including high altitude and kinetic characteristics in high-speed skip re-entry, are important for GPS positioning feasibility and were presented in accordance with the flight data. GPS solutions started at nearly 4900 km orbital altitude during the phases of re-entry process. These solutions were combined by an inertial measurement unit in a loosely coupled integrated navigation method and SINS navigation initialization. A simplified GPS/SINS navigation filter for limited resources was effectively developed and implemented on board for spacecraft application. Flight data estimation analyses, including trajectory, attitude, position distribution of GPS satellite, and navigation accuracy, were presented. The estimated accuracy of position was better than 42 m, and the accuracy of velocity was better than 0.1 m/s. 相似文献
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3.
Dong-Hwan Hwang Sang Heon Oh Sang Jeong Lee Chansik Park Chris Rizos 《GPS Solutions》2005,9(4):294-311
Due to their complementary features of GPS and INS, the GPS/INS integrated navigation system is increasingly being used for
a variety of commercial and military applications. An attitude determination GPS (ADGPS) receiver, with multiple antennas,
can be more effectively integrated with a low-cost IMU since the receiver gives not only position and velocity data but also
attitude data. This paper proposes a low-cost attitude determination GPS/INS integrated navigation system. The proposed navigation
system comprises an ADGPS receiver, a navigation computer unit (NCU), and a low-cost commercial MEMS IMU. The navigation software
includes a fault detection and isolation (FDI) algorithm for integrity. In order to evaluate the performance of the proposed
navigation system, two flight tests have been performed using a small aircraft. The first flight test confirmed the fundamental
operation of the proposed navigation system and the effectiveness of the FDI algorithm. The second flight test evaluated the
performance of the proposed navigation system and demonstrated the benefit of GPS attitude information in a high dynamic environment.
The flight test results show that the proposed ADGPS/INS integrated navigation unit gives reliable navigation performance
even when anomalous GPS data is provided and gives better navigation performance than a conventional GPS/INS unit. 相似文献
4.
多传感器与道路网数据用于汽车导航的研究 总被引：4，自引：0，他引：4
对车载导航系统中GPS接收机，车论计数器和电子罗盘传感器数据与导航电子地图所提供的道路网络数据进行了综合处理，建立了道路网络数据的网络拓扑关系，在此基础上提出了基于道路网络拓扑关系，利用GPS接收机，车轮计数器和电子罗盘传感器对汽车进行实时定位的算法。最后，对导航中汽车的定位误差进行了分析。实验证明，GPS接收机，车轮计数器和电子罗盘传感器与道路网络数据综合，在导航过程中能够补偿GPS信号技失，实时、高精度、高可靠性地确定汽车的位置。 相似文献
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针对水下机器人在浅海工作时定位误差大的问题,在浅海电磁波信号衰减不大的情况下,文中重点介绍一种基于GPS/BDS双模组合定位技术的浅海水下机器人高精度定位导航系统,为了比较双模定位系统的定位性能,设置了GPS和BDS单模定位系统作对比,提出了使用中值滤波算法和卡尔曼滤波算法相结合的定位数据处理方法,通过对双模定位系统测试数据的滤波处理,得出系统的定位性能。测试结果表明,双模定位系统的定位精度要高于单模定位系统;中值滤波和卡尔曼滤波相结合算法的应用能够明显提高双模定位系统的定位精度。 相似文献
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对北斗区域卫星导航系统（BDS）正式运行后在南极中山站地区的基本导航定位性能进行了评估,包括卫星可用性、位置精度因子（PDOP）、伪距观测值质量、电离层模型精度及单频伪距导航定位性能等方面。对南极中山站地区实测数据分析的结果表明,首先,北斗卫星导航系统的可用性与伪距观测值质量在总体上与GPS处于同一水平,并已初步具备了全天导航定位的能力,但存在卫星分布不够均匀、GEO卫星高度角较低、电离层模型精度较差等问题。其次,北斗单频伪距单点定位北、东方向的精度分别优于22 m和9 m,高程方向优于25 m;超短基线的单频伪距差分定位在北、东、高程三个方向的精度分别为3.6 m、2.3 m和3.3 m;总体而言与GPS相比有一定差距。最后,北斗/GPS组合定位相对于单一的GPS定位不仅增加了系统的可靠性,还对定位的精度有明显改善,对于单频伪距单点定位、伪距差分定位的三维点位精度可分别提高10%、22%。 相似文献
7.
A wavelet-extreme learning machine for low-cost INS/GPS navigation system in high-speed applications
The combined navigation system consisting of both global positioning system (GPS) and inertial navigation system (INS) results in reliable, accurate, and continuous navigation capability when compared to either a GPS or an INS stand-alone system. To improve the overall performance of low-cost micro-electro-mechanical systems (MEMS)-based INS/GPS by considering a high level of stochastic noise on low-cost MEMS-based inertial sensors, a highly complex problems with noisy real data, a high-speed vehicle, and GPS signal outage during our experiments, we suggest two approaches at different steps: (1) improving the signal-to-noise ratio of the inertial sensor measurements and attenuating high-frequency noise using the discrete wavelet transform technique before data fusion while preserving important information like the vehicle motion information and (2) enhancing the positioning accuracy and speed by an extreme learning machine (ELM) which has the characteristics of quick learning speed and impressive generalization performance. We present a single-hidden layer feedforward neural network which is employed to optimize the estimation accuracy and speed by minimizing the error, especially in the high-speed vehicle and real-time implementation applications. To validate the performance of our proposed method, the results are compared with an adaptive neuro-fuzzy inference system (ANFIS) and an extended Kalman filter (EKF) method. The achieved accuracies are discussed. The results suggest a promising and superior prospect for ELM in the field of positioning for low-cost MEMS-based inertial sensors in the absence of GPS signal, as it outperforms ANFIS and EKF by approximately 50 and 70%, respectively. 相似文献
8.
提高C／A码GPS接收机的定位精度对导航具有重要意义。本文利用模糊数学知识分析对定位精度影响的因素，给出隶属度函数和定位精度评估函数。对其性质进行分析，最后给出最优解的计算方法。 相似文献
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针对高精度载波相位相对定位解算的需求,研制了北斗基线解算软件BGO（BeiDou Navigation Satellite System/Global Positioning System Office）。BGO能单独处理北斗及GPS数据,也可以将北斗与GPS观测数据进行联合解算。结合一高速铁路基础平面控制网（basic plane control network,CPI）的测试表明,BGO解算北斗基线X、Y、Z方向的分量精度分别优于1 mm、2 mm、1 mm,能满足高精度高速铁路CPI控制网的要求;BGO处理GPS数据的精度与TGO（Trimble Geomatics Office）软件、Bernese软件基本一致,处理北斗与GPS联合基线性能与TBC（Trimble Business Center）软件相当。相比独立系统,联合处理北斗和GPS数据能有效提高基线解算合格率与精度。 相似文献
10.
针对微弱信号下GPS接收机无法测量得到完整信号发射时刻的问题,提出了一种基于模糊度搜索的辅助式GPS定位算法。基于该算法接收机不需要位同步、帧同步和解调导航电文,仅对GPS信号进行伪码相位测量,在获取卫星星历、卫星钟差参数等辅助信息的基础上完成定位解算。论文从数学上严格推导了消除信号发射时刻模糊度的条件,并对五颗以上的观测卫星建立了定位解算方程,给出了算法流程。利用实测数据仿真验证了该算法的有效性。比较表明,该算法的定位精度与常规GPS定位算法(信号发射时刻不存在模糊度)相当。 相似文献
11.
During past decades, precise point positioning (PPP) has been proven to be a well-known positioning technique for centimeter or decimeter level accuracy. However, it needs long convergence time to get high-accuracy positioning, which limits the prospects of PPP, especially in real-time applications. It is expected that the PPP convergence time can be reduced by introducing high-quality external information, such as ionospheric or tropospheric corrections. In this study, several methods for tropospheric wet delays modeling over wide areas are investigated. A new, improved model is developed, applicable in real-time applications in China. Based on the GPT2w model, a modified parameter of zenith wet delay exponential decay wrt. height is introduced in the modeling of the real-time tropospheric delay. The accuracy of this tropospheric model and GPT2w model in different seasons is evaluated with cross-validation, the root mean square of the zenith troposphere delay (ZTD) is 1.2 and 3.6 cm on average, respectively. On the other hand, this new model proves to be better than the tropospheric modeling based on water-vapor scale height; it can accurately express tropospheric delays up to 10 km altitude, which potentially has benefits in many real-time applications. With the high-accuracy ZTD model, the augmented PPP convergence performance for BeiDou navigation satellite system (BDS) and GPS is evaluated. It shows that the contribution of the high-quality ZTD model on PPP convergence performance has relation with the constellation geometry. As BDS constellation geometry is poorer than GPS, the improvement for BDS PPP is more significant than that for GPS PPP. Compared with standard real-time PPP, the convergence time is reduced by 2–7 and 20–50% for the augmented BDS PPP, while GPS PPP only improves about 6 and 18% (on average), in horizontal and vertical directions, respectively. When GPS and BDS are combined, the geometry is greatly improved, which is good enough to get a reliable PPP solution, the augmentation PPP improves insignificantly comparing with standard PPP. 相似文献
12.
卫星导航信号模拟源为用户终端设备的设计、验证、测试提供输入信号源,是用户终端设备研发和卫星导航信号系统验证的重要工具.早期的射频合成技术产生的信号的精度和通道一致性较差,随后的模拟中频合成技术存在通道间偏差的问题,而目前常用的数字中频合成技术存在相位抖动问题,所以本文基于PXI Express(PXIe)总线的软件无线电架构,设计并实现了一款采用数字基带合成技术的软硬件结合模拟源.模拟源上位机数学仿真软件采用图形化编程语言LABVIEW开发,实现简单,开发效率高,最终生成数字基带合成信号;模拟源硬件则使用美国国家仪器公司(NI)模块化的虚拟仪器,接收并处理上位机产生的数字基带合成信号,最终产生用户终端设备可以接收的全球定位系统(GPS)射频信号.利用频谱分析仪观察模拟源输出信号的频率和带宽,验证了GPS模拟源仿真信号的正确性;利用商用接收机进行定位解算,分析静态和动态场景下的信号质量、定位结果及三轴定位误差,验证了GPS模拟源仿真信号的准确性和有效性. 相似文献
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The problem of datum definition as applied to local-area geodetic networks is investigated using data collected from global navigation satellite systems (GNSS). It is shown that the process of double differencing makes the model more sensitive to computational errors that reduce the ability of the satellites alone to control the translation component of the datum definition, and as a result additional regularization is required. Traditionally, datum definition has been accomplished by constraining one station to set coordinates. Alternative regularization strategies are analysed in terms of their effects on positioning and ambiguity resolution. In doing so, processing strategies are developed which can improve the quality of global positioning system (GPS)-based position solutions in geodetic network applications of limited spatial extent, such as high-precision engineering and deformation monitoring networks. 相似文献
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M. R. Mosavi 《GPS Solutions》2006,10(2):97-107
Position information obtained from standard global positioning system (GPS) receivers has time variant errors. For effective use of GPS information in a navigation system, it is essential to model these errors. A new approach is presented for improving positioning accuracy using neural network (NN), fuzzy neural network (FNN), and Kalman filter (KF). These methods predict the position components’ errors that are used as differential GPS (DGPS) corrections in real-time positioning. Method validity is verified with experimental data from an actual data collection, before and after selective availability (SA) error. The result is a highly effective estimation technique for accurate positioning, so that positioning accuracy is drastically improved to less than 0.40 m, independent of SA error. The experimental test results with real data emphasize that the total performance of NN is better than FNN and KF considering the trade-off between accuracy and speed for DGPS corrections prediction. 相似文献
15.
伽利略系统(Galileo)是由欧洲独立研制开发的新一代全球卫星导航定位系统,该系统于2002年3月26日正式启动,是一个能够提供高精度的全球定位服务的完全民用系统。随着Galileo系统的建成、完全运行和GPS的现代化,人们用来导航、定位和授时的载波频率增加到7个。为了更好利用Galileo系统的4个频率的载波,有效地削弱电离层延迟等多种测量误差的影响,更快地确定整周模糊度,从而提高定位精度和可靠性,本文主要讨论了Galileo系统的观测值方程的表达式,非差组合观测值的定义、双差组合观测值的定义及相应的组合标准。 相似文献
16.
A combined algorithm of improving INS error modeling and sensor measurements for accurate INS/GPS navigation 总被引：1，自引：1，他引：1
Although the integrated system of a differential global positioning system (DGPS) and an inertial navigation system (INS)
had been widely used in many geodetic navigation applications, it has sometimes a major limitation. This limitation is associated
with the frequent occurrence of DGPS outages caused by GPS signal blockages in certain situations (urban areas, high trees,
tunnels, etc.). In the standard mechanization of INS/DGPS navigation, the DGPS is used for positioning while the INS is used
for attitude determination. In case of GPS signal blockages, positioning is provided using the INS instead of the GPS until
satellite signals are obtained again with sufficient accuracy. Since the INS has a very short-time accuracy, the accuracy
of the provided INS navigation parameters during these periods decreases with time. However, the obtained accuracy in these
cases is totally dependent on the INS error model and on the quality of the INS sensor data. Therefore, enhanced navigation
parameters could be obtained during DGPS outages if better inertial error models are implemented and better quality inertial
measurements are used. In this paper, it will be shown that better INS error models are obtained using autoregressive processes
for modeling inertial sensor errors instead of Gauss–Markov processes that are implemented in most of the current inertial
systems and, on the other hand, that the quality of inertial data is improved using wavelet multi-resolution techniques. The
above two methods are discussed and then a combined algorithm of both techniques is applied. The performance of each method
as well as of the combined algorithm is analyzed using land-vehicle INS/DGPS data with induced DGPS outage periods. In addition
to the considerable navigation accuracy improvement obtained from each single method, the results showed that the combined
algorithm is better than both methods by more than 30%. 相似文献
17.
In the complex urban environments, land vehicle navigation purely relying on GNSS cannot satisfy user needs due to the loss of satellite signals caused by obstructions such as buildings, tunnels, and trees. To solve this problem, we introduce a GPS-/MSINS-/magnetometer-integrated urban navigation system based on context awareness. In this system, the data from the Micro Strapdown Inertial Navigation System (MSINS) are used to analyze and detect the context knowledge of vehicles, whose sensor errors can be compensated by the heuristic drift reduction algorithm for different motion situations. When GPS is available, the vehicle position can be estimated by unscented Kalman Filter, whereas in the case of GPS outages, the vehicle attitude is provided by an attitude and heading reference system and the motion constraints-aided algorithm is used to complete the positioning. In the experiment validation, the integrated navigation system is set up by low-cost inertial sensors. The result shows that the proposed system can achieve high accuracy when GPS is available. For most of the time without GPS, the system can guarantee the positioning precision of 10 m and compensate the errors of MSINS effectively, which fully satisfies positioning needs in complex urban environments. 相似文献
18.
一种基于改进UKF滤波的GPS+PDR组合定位方法 总被引：1，自引：0，他引：1
针对接收信号质量恶化的环境,提出了一种适用于信号遮蔽环境的改进GPS+PDR组合定位算法。该方法用短时间内的陀螺仪积分数据校正数字罗盘的航向偏差,在一定程度上消除了数字罗盘受到的偶发干扰。采用约束残差的无迹卡尔曼滤波（UKF）算法对GPS和行人航迹推算（PDR）定位信息进行融合处理,有效克服了PDR定位中累积航向误差产生的位置漂移问题,提高了算法的定位精度和稳定性。试验结果表明,改进算法能有效抑制数字罗盘的漂移误差,航向相对误差平均降低56%;行人步行时,GPS定位标准误差为2.67 m,单纯PDR定位标准误差为6.83 m;随机给予若干点GPS数据辅助定位,标准误差降至3.12 m;全程融合GPS与PDR定位,标准误差可降至1.94 m。 相似文献
19.
基于伪卫星的改善GPS几何精度因子的研究 总被引：1，自引：1，他引：0
随着人们活动范围的日益扩大和周边环境的日益复杂,高精度GPS导航技术逐渐成为国内外研究的重点。GPS系统的定位精度在很大程度上取决于参与定位卫星的数目和几何布局,而几何精度因子(GDOP)正是衡量定位卫星几何布局优劣的量度。文章从几何精度因子着手,从理论上证明了伪卫星对GPS系统GDOP的改善,分析了伪卫星数量对GPS系统定位精度的影响。借助于仿真实验,结果表明,在GPS导航定位中,伪卫星能够显著增强卫星几何图形结构、提高测量精度、改善精度因子从而提高定位精度。 相似文献
20.
介绍车载导航定位系统的组成,比较几种导航方法的优缺点,得出几种较为合理、精度较高的组合定位方法.GPS卫星信号所包含的定位信息有其特定的格式,通过编写程序将其中所需的定位信息提取出来,并利用七参数转换方法将GPS定位系统应用的WGS-84坐标系转换成国家大地坐标系.通过车载导航试验实例分析表明,利用最短距离投影法得到的电子地图精度较高. 相似文献