共查询到20条相似文献，搜索用时 15 毫秒
1.
Ben K. H. Soon Steve Scheding Hyung-Kuen Lee Hung-Kyu Lee Hugh Durrant-Whyte 《GPS Solutions》2008,12(4):261-271
This paper presents a simple and effective approach that incorporates single-frequency, L1 time-differenced GPS carrier phase
(TDCP) measurements without the need of ambiguity resolution techniques and the complexity to accommodate the delayed-state
terms. Static trial results are included to illustrate the stochastic characteristics and effectiveness of the TDCP measurements
in controlling position error growth. The formulation of the TDCP observation model is also described in a 17-state tightly-coupled
GPS/INS iterative, extended Kalman filter (IEKF) approach. Preliminary land vehicle trial results are also presented to illustrate
the effectiveness of the TDCP which provides sub-meter positional accuracies when operating for more than 10 min. 相似文献
2.
3.
GPS／INS组合导航系统的Matlab／Simulink仿真 总被引：7，自引：1，他引：7
首先系统研究了GPS／INS组合导航系统的仿真原理，然后以Matlab／Simulink为平台，在对GPS、INS进行单独仿真的基础上，对GPS／INS组合导航系统进行了实时的扩展Kalman滤波仿真试验，试验结果不仅证明组合导航具有较高的导航精度，而且为进一步研究组合导航系统开辟了一条比较实用的道路。 相似文献
4.
在提出单历元解算GPS模糊度技术的基础上 ,使用INS间接法误差模型 ,提出了一种GPS双差载波相位多普勒 /INS全组合Kalman滤波的新方法 ,高精度直接解算机载TLS中的外方位元素。仿真数据试验表明 ,其姿态精度高于 1 0″,位置精度高于 1 0cm。 相似文献
5.
Hung Lee Jinling Wang Chris Rizos Dorota Grejner-Brzezinska Charles Toth 《GPS Solutions》2002,6(1-2):34-46
This paper discusses the introduction of pseudolites (ground-based GPS-like signal transmitters) into existing integrated
GPS/INS systems in order to provide higher availability, integrity, and accuracy in a local area. Even though integrated GPS/INS
systems can overcome inherent drawbacks of each component system (line-of-sight requirement for GPS, and INS errors that grow
with time), performance is nevertheless degraded under adverse operational circumstances. Some typical examples are when the
duration of satellite signal blockage exceeds an INS bridging level, resulting in large accumulated INS errors that cannot
be calibrated by GPS. Such a scenario, unfortunately, is a common occurrence for certain kinematic applications. To address
such shortcomings, both pseudolite/INS and GPS/pseudolite/INS integration schemes are proposed here. Typically, the former
is applicable for indoor positioning where the GPS signal is unavailable for use. The latter would be appropriate for system
augmentation when the number and geometry of visible satellites is not sufficient for accurate positioning or attitude determination.
In this paper, some technical issues concerned with implementing these two integration schemes are described, including the
measurement model, and the appropriate integration filter for INS error estimation and correction through GPS and pseudolite
(PL) carrier phase measurements. In addition, the results from the processing of simulated measurements, as well as field
experiments, are presented in order to characterize the system performance. As a result, it has been established that the
GPS/PL/INS and PL/INS integration schemes would make it possible to ensure centimeter-level positioning accuracy even if the
number of GPS signals is insufficient, or completely unavailable.
Electronic Publication 相似文献
6.
7.
针对车载全球导航卫星系统/惯性导航系统（global navigation satellite system/inertial navigation system,GNSS/INS）组合导航中卫星信号中断,惯性导航系统单独导航误差积累较大的问题,提出了附加载体运动条件约束的卡尔曼（Kalman）滤波解算方法。通过利用载体固有的运动约束,包括近似高程约束、近似速度约束和近似姿态约束,减少载体自由度和模型参数;通过引入新的观测类型,增加观测冗余,可以加强Kalman滤波解,提高在GNSS信号中断时组合导航系统的定位精度,实现无缝导航。 相似文献
8.
The architecture of the ultra-tight GPS/INS/PL integration is the key to its successful performance; the main feature of this
architecture is the Doppler feedback to the GPS receiver tracking loops. This Doppler derived from INS, when integrated with
the carrier tracking loops, removes the Doppler due to vehicle dynamics from the GPS/PL signal thereby achieving a significant
reduction in the carrier tracking loop bandwidth. The bandwidth reduction provides several advantages such as: improvement
in anti-jamming performance, and increase in post correlated signal strength which in turn increases the dynamic range and
accuracy of measurements. Therefore, any degradation in the derived Doppler estimates will directly affect the tracking loop
bandwidth and hence its performance. The quadrature signals from the receiver correlator, I (in-phase) and Q (quadrature),
form the measurements, whereas the inertial sensor errors, position, velocity and attitude errors form the states of the complementary
Kalman filter. To specify a reliable measurement model of the filter for this type of integrated system, a good understanding
of GPS/PL signal characteristics is essential. It is shown in this paper that phase and frequency errors are the variables
that relate the measurements and the states in the Kalman filter. The main focus of this paper is to establish the fundamental
mathematical relationships that form the measurement model, and to show explicitly how the system error states are related
to the GPS/PL signals. The derived mathematical relationships encapsulated in a Kalman filter, are tested by simulation and
shown to be valid.
相似文献
| Ravindra Babu (Corresponding author)Email: |
| Jinling WangEmail: |
9.
In federated design of ultra-tight GPS/INS integrated system, the baseband signal pre-processing is completed in a single pre-filter assigned for each channel. As the state space model of this single pre-filter includes the code tracking errors coupled with carrier tracking errors, ionospheric errors and normalized signal amplitude, the carrier tracking process may be destroyed. Also, the measurement noises are not independent any longer after passing through the code and carrier discriminators. Therefore, we propose a double-filter-based pre-filter model that distributes the carrier and code tracking into two independent filters: a conventional pre-filter, where the normalized signal amplitude is excluded from the state space and tracks only the code signal, and a 3-dimension state filter, tracking the carrier signal. The measurement information from both filters is a scalar quantity, which removes most of the noise correlation. To further improve the performance of the double-filter-based pre-filter model, we propose a modified Kalman filter algorithm. Simulation and field tests have been conducted, and the performance analysis has been done for the following configurations in a vector-tracking mode: double-filter model with modified Kalman filter, double-filter model with conventional Kalman filter and traditional single-filter model. The preliminary analysis indicates that the double-filter model with modified Kalman filter shows the best performance in tracking and navigation domains, while the traditional single-filter model shows a sub-optimal performance. 相似文献
10.
简要介绍了GPS/INS松组合导航系统状态方程和观测方程。针对标准Kalman滤波算法存在的状态方程截断误差、噪声统计特性的不确定性以及状态扰动异常的影响,给出了一种应用于GPS/INS组合导航系统的迭代滤波算法。该算法采用迭代策略,不断利用观测信息实时修正状态预报值。实测数据计算结果表明,通过对状态预报值的实时修正,该算法能够很好地抑制状态预报信息的不确定性和扰动异常等对导航解的影响。其滤波解精度明显优于标准Kalman滤波。 相似文献
11.
Differential carrier phase observations from GPS (Global Positioning System) integrated with high-rate sensor measurements,
such as those from an inertial navigation system (INS) or an inertial measurement unit (IMU), in a tightly coupled approach
can guarantee continuous and precise geo-location information by bridging short outages in GPS and providing a solution even
when less than four satellites are visible. However, to be efficient, the integration requires precise knowledge of the lever
arm, i.e. the position vector of the GPS antenna relative to the IMU. A previously determined lever arm by direct measurement
is not always available in real applications; therefore, an efficient automatic estimation method can be very useful. We propose
a new hybrid derivative-free extended Kalman filter for the estimation of the unknown lever arm in tightly coupled GPS/INS
integration. The new approach takes advantage of both the linear time propagation of the Kalman filter and the nonlinear measurement
propagation of the derivative-free extended Kalman filter. Compared to the unscented Kalman filter, which in recent years
is typically used as a superior alternative to the extended Kalman filter for nonlinear estimation, the virtue of the new
Kalman filter is equal estimation accuracy at a significantly reduced computational burden. The performance of the new lever
arm estimation method is assessed with simulated and real data. Simulations show that the proposed technique can estimate
the unknown lever arm correctly provided that maneuvers with attitude changes are performed during initialization. Field test
results confirm the effectiveness of the new method. 相似文献
12.
M. S. Senobari 《Journal of Geodesy》2010,84(5):277-291
A method for airborne vector gravimetry has been developed. The method is based on developing the error dynamics equations
of the INS in the inertial frame where the INS system errors are estimated in a wave estimator using inertial GPS position
as update. Then using the error-corrected INS acceleration and the GPS acceleration in the inertial frame, the gravity disturbance
vector is extracted. In the paper, the focus is on the improvement of accuracy for the horizontal components of the airborne
gravity vector. This is achieved by using a decoupled model in the wave estimator and decorrelating the gravity disturbance
from the INS system errors through the estimation process. The results of this method on the real strapdown INS/DGPS data
are promising. The internal accuracy of the horizontal components of the estimated gravity disturbance for repeated airborne
lines is comparable with the accuracy of the down component and is about 4–8 mGal. Better accuracy (2–4 mGal) is achieved
after applying a wave-number correlation filter (WCF) to the parallel lines of the estimated airborne gravity disturbances. 相似文献
13.
GPS/MEMS INS integrated system for navigation in urban areas 总被引：1，自引：2，他引：1
This paper evaluates the performance of a tightly coupled GPS/INS integrated system based on low cost MEMS IMUs in dense urban
areas, and investigates two different methods to improve its performance. The first method used is to derive observations
from two different constraint equations reflecting the behavior of a typical land vehicle. The first constraint equation is
derived assuming that the vehicle does not slip and always remains in contact with the ground. If these assumptions are true
the velocity of the vehicle in the plane perpendicular to the forward direction should be zero. The second constraint equation
is derived from the fact that the height does not change much in a short time interval in a land vehicular environment. Thus,
when a GPS outage occurs (partial/complete), the integrated system combines the INS and constraints-derived virtual measurements
to keep the position and velocity errors bounded. This method is suitable for use in real-time applications. The second method
is specifically suitable for a post-mission application and involves the use of Rauch-Tung-Striebel (RTS) smoother. The designed
system performance is evaluated using two data sets collected in dense urban areas. The obtained results demonstrate the effectiveness
of different algorithms considered, in controlling the INS error growth, and indicates the potential of MEMS IMUs for use
in land vehicle navigation applications. 相似文献
14.
研究了静止条件下零角度修正在GNSS/INS组合导航中的应用。分析了静止条件下载体航向角解算漂移的原因,给出零角度修正的具体表达式。通过更改卡尔曼滤波量测方程的方法实现航向角误差修正,并用实测数据进行实验验证。结果表明,在静止条件下单独使用零角度修正可以提高载体的航向角精度,并利于垂向陀螺零偏的估计;在零角度修正基础上结合零速修正技术,航向角精度可以进一步改善。 相似文献
15.
扩展区间Kalman滤波器及其在GPS/INS组合导航中的应用 总被引：16，自引：1，他引：15
针对具有不确定动态模型参数的 GPS/INS 组合导航系统,首先介绍一种新型的区间Kalman滤波器,讨论了GPS/INS 组合系统中模型参数不确定性的问题,分析了惯性传感器建模中相关时间常数的区间特性,并建立了适合非线性特性的GPS/INS组合系统的扩展区间卡尔曼滤波器.计算结果表明,扩展区间卡尔曼滤波器对非线性GPS/INS组合系统是很有效的,它能给出组合系统导航误差的上下界,这对组合系统的设计具有指导的意义. 相似文献
16.
Ionospheric correction using NTCM driven by GPS Klobuchar coefficients for GNSS applications 总被引：1，自引：1，他引：0
Global Navigation Satellite Systems (GNSS) require mitigation of ionospheric propagation errors because the ionospheric range errors might be larger than tens of meters at the zenith direction. Taking advantage of the frequency-dispersive property of ionospheric refractivity, the ionospheric range errors can be mitigated in dual-frequency applications to a great extent by a linear combination of carrier phases or pseudoranges. However, single-frequency GNSS operations require additional ionospheric information to apply signal delay or range error corrections. To aid single-frequency operations, the global positioning system (GPS) broadcasts 8 coefficients as part of the navigation message to drive the ionospheric correction algorithm (ICA) also known as Klobuchar model. We presented here an ionospheric correction algorithm called Neustrelitz TEC model (NTCM) which can be used as complementary to the GPS ICA. Our investigation shows that the NTCM can be driven by Klobuchar model parameters to achieve a significantly better performance than obtained by the mother ICA algorithm. Our research, using post-processed reference total electron content (TEC) data from more than one solar cycle, shows that on average the RMS modeled TEC errors are up to 40% less for the proposed NTCM model compared to the Klobuchar model during high solar activity period, and about 10% less during low solar activity period. Such an approach does not require major technology changes for GPS users rather requires only introducing the NTCM approach a complement to the existing ICA algorithm while maintaining the simplicity of ionospheric range error mitigation with an improved model performance. 相似文献
17.
载波平滑伪距技术是一种有效的GNSS数据处理技术,在很多高精度实时定位场合得到了广泛的应用。本文在随机模型中考虑载波相位时间差分观测量中有限冲激响应有色观测噪声的影响,推导出采用递归最小二乘方法的距离域和位置域双频载波相位平滑伪距算法,并利用实测数据验证了新算法的有效性。试验表明,相位平滑伪距能够减小伪距观测值的误差,提高伪距观测量的精度,从而提高定位精度;相对于传统的算法,距离域与位置域滤波的伪距平滑精度均有提高,三维定位误差精度均得到改善;同时表明,载波相位时间差分的有色噪声对平滑效果和定位精度有一定的影响。 相似文献
18.
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
19.
20.
设计了一套基于集中式卡尔曼滤波的实时动态定位（real-time kinematic,RTK）/惯性导航系统（inertial navigation system,INS）紧组合算法,通过实测车载数据对比分析了3颗可用卫星时的固定解和浮点解在位置漂移误差水平和模糊度恢复时间上的差异,验证了该算法在卫星较少情况下的良好性能。该算法在即使观测卫星不足4颗时使用固定解或浮点解进行滤波更新,提高了组合导航在复杂环境下的位置精度,并加快了模糊度恢复过程。实验结果表明,使用中等精度的惯导,在可见卫星数为3颗时,失锁30 s时的水平位置漂移误差为0.3 m;失锁60 s内,平均1~2 s就能可靠地恢复整周模糊度。在位置漂移误差与模糊度恢复方面,固定解和浮点解在GNSS信号短期部分失锁时的差异并不显著,但同时都明显优于信号完全失锁情形。 相似文献