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地面车辆 SINS 与组合里程计的组合导航技术研究。

Research on the Integrated Navigation Technology of SINS with Couple Odometers for Land Vehicles.

机构信息

School of Instrumentation and Optoelectronic Engineering, Beihang University, Beijing 100191, China.

出版信息

Sensors (Basel). 2020 Jan 19;20(2):546. doi: 10.3390/s20020546.

Abstract

Autonomous and accurate acquisition of the position and azimuth of the vehicle is critical to the combat effectiveness of land-fighting vehicles. The integrated navigation system, consisting of a strap-down inertial navigation system (SINS) and odometer (OD), is commonly applied in vehicles. In the SINS/OD integrated system, the odometer is installed around the vehicle's wheel, while SINS is usually installed on the base of the vehicle. The distance along SINS and OD would cause a velocity difference when the vehicle maneuvers, which may lead to a significant influence on the integration positioning accuracy. Furthermore, SINS navigation errors, especially azimuth error, would diverge over time due to gyro drifts and accelerometer biases. The azimuth error would cause the divergence of dead-reckoning positioning errors with the distance that the vehicle drives. To solve these problems, an integrated positioning and orientation method based on the configuration of SINS and couple odometers was proposed in this paper. The proposed method designed a high precision integrated navigation algorithm, which compensated the lever arm effect to eliminate the velocity difference between SINS and odometers. At the same time, by using the measured information of couple odometers, azimuth reference was calculated and used as an external measurement to suppress SINS azimuth error's divergence over time, thus could further improve the navigation precision of the integrated system, especially the orientation accuracy. The performance of the proposed method was verified by simulations. The results demonstrated that SINS/2ODs integrated system could achieve a positioning accuracy of 0.01% D (total mileage) and orientation accuracy of ±30″ by using SINS with 0.01°/h Fiber-Optic Gyroscope (FOGs) and 50 µg accelerometers.

摘要

自主且精确地获取车辆的位置和方位对于地面作战车辆的战斗力至关重要。捷联惯性导航系统(SINS)和里程计(OD)组成的组合导航系统通常应用于车辆中。在 SINS/OD 组合系统中,里程计安装在车辆的车轮周围,而 SINS 通常安装在车辆的基座上。当车辆进行机动时,SINS 和 OD 沿车辆行驶的距离会导致速度差异,这可能会对组合定位精度产生重大影响。此外,由于陀螺漂移和加速度计偏差,SINS 导航误差,尤其是方位误差,会随时间发散。方位误差会导致车辆行驶距离的推算定位误差发散。为了解决这些问题,本文提出了一种基于 SINS 和耦合里程计配置的组合定位和定向方法。该方法设计了一种高精度的组合导航算法,补偿了杠杆臂效应,消除了 SINS 和里程计之间的速度差异。同时,通过使用耦合里程计的测量信息,计算了方位参考值,并将其作为外部测量值,以抑制 SINS 方位误差随时间的发散,从而进一步提高组合系统的导航精度,特别是定向精度。通过仿真验证了该方法的性能。结果表明,使用具有 0.01°/h 光纤陀螺(FOG)和 50 µg 加速度计的 SINS,SINS/2ODs 组合系统可以实现 0.01% D(总里程)的定位精度和±30″的定向精度。

https://cdn.ncbi.nlm.nih.gov/pmc/blobs/ad75/7014487/b2e4cb781e3f/sensors-20-00546-g001.jpg

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