共查询到18条相似文献，搜索用时 157 毫秒
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介绍了一种组合低成本的GPS和IMU(Inertial Measurement Unit)来获得高精度姿态、位置和速度信息的方法。文中介绍了GPS／IMU组合系统的设计方案及系统的硬件和软件设计，并给出了实验结果。该组合系统将来安装于炮兵测地车后，不仅可以提高测地的精度，而且在采样率、可靠性等方面比单独采用GPS定位的方法更有优势。 相似文献
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在机场抢修抢建中,对测量系统的作业时间、定位精度、可靠性具有较高的要求,本文提出了一种新型高精度IMU/TS组合定位导航方法,引入激光跟踪定位/惯性组合导航理念,分析了系统组成以及各传感器的误差项,将系统时间延迟作为新的状态估计参数,采用卡尔曼滤波器将IMU和TS数据进行数据融合处理,并在车载动态应用条件下同IMU/GPS组合定位导航系统进行了实验数据比对,验证了在无GNSS信号环境下IMU/TS组合定位导航系统的位置测量精度。 相似文献
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研究无控制点情况下的红外影像目标快速定位技术,有利于发挥红外遥感的测绘应用潜力。首先介绍了基于GPS/IMU的目标定位原理与方法;然后实验验证了红外影像多像前方交会和GPS/IMU辅助红外影像光束法区域网平差的可行性;并分析了误差产生的原因。实验证明,航空红外遥感在GPS/IMU组合系统的配合下,能满足目标探测与预警的精度要求,具有实用价值。 相似文献
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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
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Dead reckoning techniques such as inertial navigation and odometry are integrated with GPS to avoid interruption of navigation
solutions due to lack of visible satellites. A common method to achieve a low-cost navigation solution for land vehicles is
to use a MEMS-based inertial measurement unit (IMU) for integration with GPS. This integration is traditionally accomplished
by means of a Kalman filter (KF). Due to the significant inherent errors of MEMS inertial sensors and their time-varying changes,
which are difficult to model, severe position error growth happens during GPS outages. The positional accuracy provided by
the KF is limited by its linearized models. A Particle filter (PF), being a nonlinear technique, can accommodate for arbitrary
inertial sensor characteristics and motion dynamics. An enhanced version of the PF, called Mixture PF, is employed in this
paper. It samples from both the prior importance density and the observation likelihood, leading to an improved performance.
Furthermore, in order to enhance the performance of MEMS-based IMU/GPS integration during GPS outages, the use of pitch and
roll calculated from the longitudinal and transversal accelerometers together with the odometer data as a measurement update
is proposed in this paper. These updates aid the IMU and limit the positional error growth caused by two horizontal gyroscopes,
which are a major source of error during GPS outages. The performance of the proposed method is examined on road trajectories,
and results are compared to the three different KF-based solutions. The proposed Mixture PF with velocity, pitch, and roll
updates outperformed all the other solutions and exhibited an average improvement of approximately 64% over KF with the same
updates, about 85% over KF with velocity updates only, and around 95% over KF without any updates during GPS outages. 相似文献
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A reduced inertial measurement unit (IMU) consisting of only one vertical gyro and two horizontal accelerometers or three orthogonal accelerometers can be used in land vehicle navigation systems to reduce volume and cost. In this paper, a reduced IMU is integrated with a Global Positioning System (GPS) receiver whose phase lock loops (PLLs) are aided with the Doppler shift from the integrated system. This approach is called tight integration with loop aiding (TLA). With Doppler aiding, the noise bandwidth of the PLL loop filters can be narrowed more than in the GPS-only case, which results in improved noise suppression within the receiver. In this paper, first the formulae to calculate the PLL noise bandwidth in a TLA GPS/reduced IMU are derived and used to design an adaptive PLL loop filter. Using a series of vehicle tests, results show that the noise bandwidth calculation formulae are valid and the adaptive loop filter can improve the performance of the TLA GPS/reduced IMU in both navigation performance and PLL tracking ability. 相似文献
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IMU/GPS组合导航系统自适应Kalman滤波算法 总被引：10，自引：0，他引：10
给出了IMU在地固坐标系中的误差方程，介绍并分析了自适应滤波和渐消Kalman滤波算法原理，然后将渐消因子引入到自适应滤波算法中。并将其应用到IMU／GPS松组合导航系统中，最后利用一个实际算例证明了该组合导航系统的有效性。 相似文献
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Application of Adaptive Kalman Filtering Algorithm in IMU/GPS Integrated Navigation System 总被引：5，自引：0，他引：5
GAO Weiguang YANG Yuanxi CUI Xianqiang ZHANG Shuangcheng 《地球空间信息科学学报》2007,10(1):22-26
The IMU(inertial measurement unit) error equations in the earth fixed coordinates are introduced firstly. A fading Kalman filtering is simply introduced and its shortcomings are analyzed, then an adaptive filtering is applied in IMU/GPS integrated navigation system, in which the adaptive factor is replaced by the fading factor. A practical example is given. The results prove that the adaptive filter combined with the fading factor is valid and reliable when applied in IMU/GPS integrated navigation system. 相似文献
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The application of low-cost L1 GPS receivers integrated with micro-electro-mechanical system (MEMS) inertial measurement units
(IMU) allows the continuous observation of position, velocity and orientation which opens new possibilities for comparison
of athletes’ performance throughout a racecourse. In this paper, we compare loosely and closely coupled integration strategies
under realistic racing scenarios when GPS is partially or completely masked. The study reveals that both integration approaches
have a similar performance when the satellite constellation is completed or the outages are short. However, for less than
four satellites, the closely coupled strategy clearly outperforms the loosely coupled approach. The second part of the paper
is devoted to the important problem of system initialization, because the conventional GPS/IMU alignment methods are no longer
applicable when using MEMS-IMU. We introduce a modified coarse alignment method and a quaternion estimation method for the
computation of the initial orientation. Simulations and practical experiments reveal that both methods are numerically stable
for any initial orientation of the sensors with the error characteristics of MEMS-IMUs. Throughout the paper, our findings
are supported by racing experiments with references provided in both, the measurement and the navigation domains. 相似文献
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Performance improvement of integrated Inertial Measurement Units (IMU) utilizing micro-electro-mechanical-sensors (MEMS) and
GPS is described in this paper. An offline pre-defined Fuzzy model is employed to improve the system performance. The Fuzzy
model is used to predict the position and velocity errors, which are the inputs to a Kalman Filter (KF) during GPS signal
outages. The proposed model has been verified on real MEMS inertial data collected in a land vehicle test. A number of 30-s
GPS outages were simulated during the data processing at different times and under different vehicle dynamics. Performance
of the suggested Fuzzy model was compared to that of the traditional KF particularly during the simulated GPS outages. The
test results indicate that the proposed Fuzzy model can efficiently compensate for GPS updates during short outages. 相似文献
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为了系统验证SINS／GPS紧组合系统的性能,基于GPS软件接收机,进行了仿真系统构建。仿真系统由轨迹发生器、GPS中频信号模拟器、IMU信号模拟器、GPS软件接收机、SINS导航解算模块、组合滤波算法和导航性能分析模块等部分构成,其中详细设计了GPS软件接收机中的捕获和跟踪算法、SINS解算以及基于伪距和伪距率的组合滤波算法。仿真结果表明：紧组合导航系统收敛性较好,能够一定程度上抑制惯导系统误差的积累,有较好的导航性能。设计的该系统满足紧组合导航系统性能验证的需要,也为后续的超紧组合研究奠定了良好的基础。 相似文献