Fault diagnosis method of embedded flight parameter sensing system for blunt airframe
Fault diagnosis method of embedded flight parameter sensing system for blunt airframe
- Neue Suche nach: WANG PENG
- Neue Suche nach: ZHAO JUNBO
- Neue Suche nach: WANG PENG
- Neue Suche nach: ZHAO JUNBO
The invention relates to a fault diagnosis method of an embedded flight parameter sensing system for a blunt airframe, which is accurate in fault diagnosis, not only can diagnose the condition that a pressure hole is completely invalid, but also can diagnose the condition that the pressure of the pressure hole abnormally fluctuates, namely the condition that the pressure fluctuation amplitude exceeds an algorithm error limit. The fault diagnosis reliability is high; the engineering applicability is high; the method is wide in application speed range and can be used in the fields of low speed, subsonic speed, transonic speed, supersonic speed and hypersonic speed.
本发明涉及一种钝头机体用嵌入式飞行参数传感系统的故障诊断方法，故障诊断准确，不仅可诊断测压孔完全失效的情形，同时可诊断测压孔压力异常波动的情形，即压力波动幅值超过算法误差限的情形；故障诊断可靠性高；工程适用性强；应用速域宽泛，可用于低速、亚、跨、超声速及高超声速领域。
Dokumentinformationen
Fault diagnosis method of embedded flight parameter sensing system for blunt airframe
一种钝头机体用嵌入式飞行参数传感系统的故障诊断方法
2024-04-19
Patent
Elektronische Ressource
Chinesisch
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