新方法可生成精简的、故障覆盖率高的测试图形，并尽可能多地检测多重故障。
The proposed method can generate simplified test patterns with high fault coverage, and can detect multiple faults as many as possible.
讨论了可重构飞控系统的故障可检测性、可重构性等基本概念。
The conception of failure detectability and reconfiguration are discussed for reconfigurable control system.
仿真结果表明，采用这种陀螺构型和故障检测算法，系统可检测较小幅度的软故障，从而获得优良的容错性能。
The simulation results show that the smaller soft faults can be detected and the excellent fault-tolerant performance can be obtained using this gyro configuration and the fault detection algorithm.
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