Interactive Electronic Technical Manual (IETM) serves as a key supporting technology of aeronautic equipment support informatization and is a carrier for structural, interactive and intelligent equipment technology data. In order to solve the problems that the traditional fault diagnosis system is single in diagnosis-oriented object, low in universality and insufficient in diagnosis knowledge and the like, accurate and efficient fault diagnosis can be performed by virtue of lots of fault diagnosis knowledge in aeronautic equipment IETM. However, knowledge source of the fault diagnosis knowledge exists in various systems of various stages of aeronautic equipment service life, knowledge acquisition model is established with respect to different fault diagnosis knowledge acquisition methods at various stages of study, and isomerism of each system is shielded, thereby realizing resource sharing, improving the fault diagnosis knowledge quality and providing more accurate fault diagnosis service for aeronautic equipment.

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This paper establish the function relationship between various parameters based on the study of the hydraulic pump and the dynamic characteristics. Through the establishment of transfer function is pull transform and the analysis of the characteristics of the transfer function of accumulator absorbing pressure pulsation actual effect. On the basis of further analysis, the improved method of effective volume of the accumulator, designed for fault detection and improve the system to provide a reliable basis.

Design a DC/AC converter based on simplex single voltage source high frequency pulse DC loop technology, the output is 115V400Hz, 0.9KVA and the input is three phase alternating current. The forward part is DC/DC converter which provides pulse D.C. to the back part DC/AC converter. Implement soft-switch by changing the on-off state of switching tubes on the inversion arm path at the zero-voltage instant of the pulse direct current, no need of the auxiliary resonant net. The system takes three-state DPM current hysteresis control mode, gets good performance on output wave and efficiency.

Acquiring causal knowledge of abnormity is essential to Missile-Launching reliably. There are lots of Knowledge Acquisition methods. But it is absence for usage and maintenance support process. So it is necessary to start the research on new knowledge acquisition technology of aid Decision-Making for Missile-Launching. Based on the Usage and Maintenance-Support Process, this thesis acquires knowledge with the ESD and CESD (Converse Event Sequence Diagram) method. First, this thesis gives the concept of CESD. Then, in order to adapt the CESD model of the complex systems more effectively, this paper expands the CESD framework and provides a software frame of computer aided ESD study. Finally, the operation of pulse power supply system is analyzed on the basis of the improved ESD and CESD. This sample shows the applicability of ESD and CESD methodology in knowledge acquisition technology of aid Decision-Making for Missile-Launching.