低成本IMU／GPS组合导航系统研究

ＧＰＳ／ＩＮＳ组合导航系统已在一定领域得到应用，而ＩＮＳ昂贵的价格限制了它的广泛应用，本文采用低成本惯性测量组件（ＩＭＵ）设计了低成本ＩＭＵ／ＧＰＳ组合系统的硬件和相应的软件，进行了静态实验和数据处理，系统的俯仰角和横滚角误差均小于０．２°，实验结果表明，低成本组合系统的性能较好，而其性能价格比更高。     

A Self-organizing Bearings-only Target Tracking Algorithm in Wireless Sensor Network

In the bearings-only target tracking, wireless sensor network (WSN) collects observations of the target direction at various nodes and uses an adaptive filter to combine them for target tracking. An efficient network management is necessary to gain an optimal tradeoff between locating accuracy and energy consumption. This article proposes a self-organizing target tracking algorithm to select the most beneficial subset of nodes to track the target at every snapshot. Compared with traditional methods, this scheme avoids the need for keeping global position information of the network as in greedy selection. Each node judges its future usefulness depending on the knowledge of its own position and using simple mathematics computation. Simulations indicate that this scheme has locating accuracy comparable to the global greedy algorithm. Also, it has good robustness against node failure and autonomous adaptability to the change of the network scale. Furthermore, this algorithm consumes limited energy because only a portion of nodes partakes in the selection at every snapshot.     

INVESTIGATION OF TIGHTLY COUPLED SINS/GPS INTEGRATION MIDCOURSE GUIDANCE FOR AIR-TO-AIR MISSILES

ＩＮＶＥＳＴＩＧＡＴＩＯＮＯＦＴＩＧＨＴＬＹＣＯＵＰＬＥＤＳＩＮＳ／ＧＰＳＩＮＴＥＧＲＡＴＩＯＮＭＩＤＣＯＵＲＳＥＧＵＩＤＡＮＣＥＦＯＲＡＩＲ┐ＴＯ┐ＡＩＲＭＩＳＳＩＬＥＳＦｕＬｉ（富立），ＦａｎＹａｏｚｕ（范耀祖），ＮｉｎｇＷｅｎｒｕ（宁文如）（Ｆ...     

基于比例阀控制的液压附件部件综合试验台的设计

针对某飞机液压系统对液压附件、部件的测试要求,设计了多支路液压系统综合试验台,实现了对飞机液压系统中作动器的动作时间、次数和速度等参数测试,对液压缸、阀、集成块等附件在不同压力、流量和温度等条件下的性能测试。该设计主要采用比例阀控制压力和流量,多级过滤器进行油源净化,PLC和继电器实现测控、电位计进行压力和流量调节,数显表直接显示压力、流量和温度、时间等参数。通过实际测试验证,试验台工作稳定、安全可靠、调整方便、显示直观、振动噪音小、不泄露,满足了某型号飞机液压附件部件测试的要求。     

Kalman filtering for GPS/magnetometer integrated navigation system

This paper investigated the data processing method for a GPS/IMU/magnetometer integrated system with Kalman filtering (KF). As a result of GPS/IMU/magnetometer land vehicle system, dead-reckoning of magnetometer and accelerometer integrated subsystem bridged very well the GPS signal outage due to the trees on the two sides of the road. Both differential GPS data processing method and the carrier-phase method with magnetometers’ outputs for predicting the car position, velocity, and acceleration (PVA) are presented. The results from DGPS with Kinematical Positioning (KINPOS) software shown that the averages of the north, east, and down direction standard deviation (short for “std”) are 0.014, 0.010, and 0.018 m, respectively. The std of velocities and accelerations derived by the position and velocity differentiation are 10, 7, 13 mm/s, 7, 5, 9 mm/s², respectively. This method for getting velocities and accelerations requires higher accurate position coordinates. But the position accuracy has frequently been degraded in this case when the car drove under the trees or other similar kinematical environments. That caused the larger velocity and acceleration errors. While the results from the carrier-phase method are std of the velocities = 2.1 mm/s, 1.3 mm/s, 3.7 mm/s in north, east, down, and std of the accelerations = 1.5 mm/s², 0.9 mm/s², 2.3 mm/s² for the static test period; as compared with KINPOS software results, std of the velocity difference between the carrier-phase method and the DGPS method = 7 mm/s, 6.9 mm/s, 9.7 mm/s in north, east, down direction, and std of acceleration difference = 5.0 mm/s², 4.5 mm/s², 7.5 mm/s² in north, east, down direction for the kinematical test period. Obviously, errors come from both the carrier-phase method and DGPS velocity and acceleration results derived directly by the position differentiation. In addition, better accuracy of positions than that before KF has been got by means of velocities and accelerations derived by the carrier-phase method after KF.     

Specification of the Earth’s plasmasphere with data assimilation

In this paper we report on initial work toward data assimilative modeling of the Earth’s plasmasphere. As the medium of propagation for waves which are responsible for acceleration and decay of the radiation belts, an accurate assimilative model of the plasmasphere is crucial for optimizing the accurate prediction of the radiation environments encountered by satellites. On longer time-scales the plasmasphere exhibits significant dynamics. Although these dynamics are modeled well by existing models, they require detailed global knowledge of magnetospheric configuration which is not always readily available. For that reason data assimilation can be expected to be an effective tool in improving the modeling accuracy of the plasmasphere. In this paper we demonstrate that a relatively modest number of measurements, combined with a simple data assimilation scheme, inspired by the ensemble Kalman filtering data assimilation technique does a good job of reproducing the overall structure of the plasmasphere including plume development. This raises hopes that data assimilation will be an effective method for accurately representing the configuration of the plasmasphere for space weather applications.     

时频域滤波方法及其在颤振信号处理中的应用

采用自适应时频分析方法并通过理论分析和数字仿真完成了相应的数值特性与应用特性研究。根据颠振试验的原理和观测信号特点，将所提出的两种时频域滤波算法引入到了飞机结构亚临界响应分析的颠振边界预测研究当中，即通过联合时频分析(JTFA)与时频域滤波提取有效信号再进行模态参数提取与颠振边界预测，取得了预期的效果。     

分散信息滤波及其在组合导航中的应用

 本文提出一种分级式分敞信息滤波算法,并通过具体实例研究了它在组合导航系统中的应用。这种算法的特点是主滤波器的计算量小,量测修正只涉及到加(减)法运算。尤其适合于数据采样频率较高、反馈校正间隔较长的组合导航系统。     

飞行控制系统舵面效率损失率估算方法研究

以某型飞机为研究对象，论述了一种基于模型的自修复飞行控制系统舵面效率损失率的估算方法。首次提出了采用多传感器信息融合来估算舵面效率损失率。因为舵面损伤故障采用全局滤波法检测，没有可直接测量其损伤程度的传感器，所以需要从飞控系统中多个传感器的测量信号综合判决来估算舵面损伤情况。最后，对所设计的舵面效率损失率的估算方法进行了数字仿真研究。仿真结果验证了该方法具有较高的准确性和实时性，为飞行控制系统舵面效率损失率的估算提供了一种有效的方法。     

浅谈电磁兼容技术

本文简单介绍了电磁兼容基本原理、电磁干扰与消除办法。