| 摘要 |
<p>The present invention relates to control systems intended for use in complex technical objects that operate in a wide range of modes and loads, wherein said invention can be used in the control systems of jet engines, power-plant turbines, etc. The method of the present invention involves connecting sensors (3) to the condition monitoring units which are designed according the model of the engine (object) (1), and connecting all sensors but one to the remaining monitoring units. The method involves calculating the weighted sum of the square values of the offsets between all condition monitoring units, and comparing the values of the weighted sum of the square values of the offsets in a first unit with the values of the weighted sums of the square values of the offsets in each of the remaining monitoring units. The maximal value among the values of the difference signals obtained is compared with a threshold value and, in case said value exceeds the threshold value, a failure signal is generated for that sensor (3) whose parameters are not used in the operation monitoring unit. The method further involves determining for each monitoring unit the potential location area of the offsets due to parametering errors of the object model, and determining those monitoring units whose offsets exceed the limits of a predetermined area.</p> |
