基于MEMS的GPS/SINS组合导航技术发展现状

对比了GPS、捷联式惯导系统、微电子机械系统(MEMS)惯性传感器各自的优缺点.针对目前以惯性技术为基础的组合导航系统得到了重视和发展,介绍了基于MEMS的GPS/捷联式惯导组合过程中存在的各种技术问题和解决这些技术难题的技术途径.     

捷联惯导系统中微机械陀螺测试参数的分析与标定

提出一种对微机械陀螺捷联惯性组件测试的方法,特点在于操作易于实现、校准方法简单、校准精度较高.实验结果表明,测试方法切实可行,整个测试过程所需的时间短,具有较高的工程使用价值.     

基于MEMS的温度数据采集系统的设计

基于数字温度传感器DS18B20的数据采集系统具有微型化,智能化,集成化的特点,介绍了此系统的结构,硬件和软件设计.DS18B20作为微传感器,其使用大大降低了系统的功耗和成本.该系统功耗低,结构简单,性能稳定,可靠性高,具有很高的使用价值.     

Dynamic Analysis of Micro-machined Diamagnetic Stable Permanent Magnet Levitation System

A novel micro-machined diamagnetic stable levitation system (MDSLS) which is composed of a free permanent magnetic rotor, a ring lifting permanent magnet and two diamagnetic stabilizers was presented. The static and dynamic stable characters of MDSLS were analyzed. The coupled non-linear differential equations were used to describe six-degree-of-freedom motion of the levitated rotor, and the equivalent surface current and combined diamagnetic image current method were utilized to model the interaction forces and torques between the lifting permanent magnet and rotor permanent magnet and also between the rotor permanent magnet and diamagnetic substrates. Because of difficulty to get analytical solution, the numerical calculation based on Runge-Kutta method was used to solve the dynamic model. The vibration frequencies were identified by fast Fourier transform (FFT) analysis. According to their resonance characteristics and parameters, the translational and angular dynamic stiffness were also calculated. The results show that the levitation of the rotor in MDSLS is stable, and the MDSLS is potential for the application in levitation inertial sensor.     

船舶MEMS微惯导网络精度技术研究

为了减少误差积累,提高导航精度,通过船舶上的CAN总线网络,利用高精度主惯导系统对低精度的MEMS微惯导系统进行在线修正。根据微惯导网络系统姿态角的误差模型,将惯导系统的角速率输出值作为量测信息设计卡尔曼滤波器,对姿态角修正算法进行了仿真运算,估计出了MEMS微惯导系统姿态角误差。     

Measurement and analysis of tyre and tread block dynamics due to contact phenomena

This paper deals with the dynamic behaviour of tyres and it is aimed at describing their dynamic features in the frequency band above 1 kHz, a range difficult to manage due to measurement noise and to the unreliability of numerical models, where the main influence is that of tread and blocks. Measurements have been made possible by fixing three three-axial micro-electro-mechanical system accelerometers on the liner and exciting the tyre under test by means of a dedicated test bench, suitably designed and constructed. Different kinds of tests have been considered in this research and described in the present paper. All of them show that a strong link exists between contact phenomena and tyre response in the frequency band over 1 kHz. This field is dominated by the tread and block dynamic responses. Furthermore, it is shown that vibrations of a sliding tyre give contributions in that frequency range for the above-mentioned reasons. It is thought that the study of the tyre behaviour over 1 kHz, though affected by significant uncertainties, can provide a proper knowledge to improve breaking effectiveness.     

Micro-electro-mechanical-sensor inertial navigation system-assisted global navigation satellite system receiver acquisition scheme and performance evaluation

When an aircraft moves under a low carrier-to-noise ratio (CNR) or at a high speed, increasing the sensitivity of global navigation satellite system (GNSS) receiver is a goal quite hard to achieve. A novel acquisition scheme assisted with micro-electro-mechanical-sensor (MEMS) inertial navigation system (INS) is presented to estimate the Doppler caused by user dynamics relative to each satellite ahead of time. Based on tightly coupled GNSS/INS estimation algorithm, MEMS INS Doppler error that can be achieved is first described. Then, by analyzing the mean acquisition time and signal detection probability, the MEMS INS-assisted acquisition capabilities in cold, warm and hot starts are quantitatively determined and compared with the standard GNSS acquisition capability. The simulations and comparisons have shown that: the acquisition time in cold start can be shortened by at least 23 s, the time in warm start can be shortened to 1 s and the acquisition capability is improved 95%, and the reacquisition time in hot start can be shortened by around 0.090 s and the capability can be enhanced 40%. The results demonstrate the validity of the novel method.