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基于在线模型的飞控系统传感器的故障诊断 被引量:9

Fault Diagnosis of Sensors of Flight Control System Based on Analytical Model
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摘要 传感器是测量无人机姿态信息的核心,传感器为无人机的飞行提供安全、可靠、全面的数据信息。飞机的安全很大程度上取决于传感器是否故障。故障诊断技术的研究,有利于提高飞行器的运行安全可靠性。首先,对无人机机载传感器的工作原理进行分析,在此基础上建立无人机执行机构的解析模型。以模型为依据,对无人机的传感器进行特性仿真。其次,利用了一种基于残差的阈值-改进SPRT联合诊断算法,从残差中提取故障特征,对传感器的工作状态做出检测和判断。最后,建立了传感器故障常见的数学模型,亦对传感器故障特性进行仿真验证。结果表明,这种方案能有效提高传感器故障的诊断精度,故障诊断算法有效。 Being the core for attitude information measurement, the sensors onboard UAV can supply safe, reliable and comprehensive information, and their working status directly affects the safety of the plane. By means of fault diagnosis technology, we can realize early detection of faults, thus to avoid malignant accidents and enhance the operation safety and reliability of aircraft. In this paper, analysis is made to the working principle of the sensors onboard the UAV, and an analytical model of the execution mechanism of the UAV is established. Based on the model, the characteristics of the sensors are simulated. Then, a fault diagnosis algorithm, threshold-improved SPRT united ALG based on residual errors, is used for extracting the fault features from residual errors, thus to detect and determine the working status of sensors. Finally, a common mathematical model of actuator's fault is established, and the fault characteristics of the sensor are simulated. The result shows that this scheme can effectively improve the accuracy of sensor fault diagnosis, and the fault diagnosis algorithm is effective.
出处 《电光与控制》 北大核心 2017年第7期81-84,94,共5页 Electronics Optics & Control
关键词 飞控系统 传感器 解析模型 故障诊断 flight control system sensor analytical model fault diagnosis
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  • 1李渭华,萧德云,方崇智.基于δ算子的格形故障检测滤波器[J].自动化学报,1994,20(4):413-419. 被引量:11
  • 2李渭华,萧德云,方崇智.一种基于自适应滑动窗格形滤波算法的故障检测器[J].自动化学报,1996,22(2):251-253. 被引量:7
  • 3Fisher K A,Maybeck P S.Multiplemodel adaptive estimation with filter spawning[J].IEEE Trans on Aerospace and Electronic Systems,2002,38(3):755-768.
  • 4Menke T E,Maybeck P S.Sensor/actuator failure detection in the vista F-16 by multiple model adaptive estimation[J].IEEE Trans on Aerospace and Electronic Systems,1995,31(4):1218-1229.
  • 5Zhang Y M,Jiang J.Integrated active fault-tolerant control using IMM Approach[J].IEEE Trans Aerospace and Electronic Systems,2001,37(4):1221-1235.
  • 6Zhang Y,Jiang J.Active fault-tolerant control system against partial actuator failures[J].IEE Proceedings Control Theory Applications,2002,149(1):95-104.
  • 7Jiang B,Staroswiecki M,Cocquempot V.Robust fault diagnostic filter design for bilinear stochastic systems[J].Control and Intelligent Systems,2001,29(1):1-7.
  • 8Gang T,Chen S H,Josh S M.An adaptive actuator failure compensation controller using output feedback[J].IEEE Trans on Automatic Control,2002,47(3):506-511.
  • 9[2]Patton R J,Frank P M,Clark R N. Issue of fault diagnosis for dynamic systems[M]. Berlin:Springer Verlag, 2000.
  • 10[3]Patan K. Fault detection of the actuators using neural networks[A]. Proceedings of the 7th IEEE International Conference on Methods and Models in Automation and Robotics[C]. Porland:IEEE, 2001.1085-1090.

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