CAJ | 학술논문

　　随着航空电子系统的飞速发展，系统对通用处理模块的功能性要求不断增加，通用处理模块的硬件功能集成化程度不断提高。文章采用硬件功能分区的方法实现了某航空显示控制系统通用处理模块的高度集成化、通用化、模块化设计，通过FPGA和应用软件的可配置实现系统要求的各种功能，可实现模块级故障的检测与隔离。经系统仿真测试和系统实物飞行试验测试验证，通用处理模块性能满足系统指标要求，并且系统的体积、重量、功耗明显减小，可靠性得到了提高。
　　수착항공전자계통적비속발전，계통대통용처리모괴적공능성요구불단증가，통용처리모괴적경건공능집성화정도불단제고。문장채용경건공능분구적방법실현료모항공현시공제계통통용처리모괴적고도집성화、통용화、모괴화설계，통과FPGA화응용연건적가배치실현계통요구적각충공능，가실현모괴급고장적검측여격리。경계통방진측시화계통실물비행시험측시험증，통용처리모괴성능만족계통지표요구，병차계통적체적、중량、공모명현감소，가고성득도료제고。
At present, the design of aviation display and control system is getting more comprehensive and highly integrated. The corresponding result is that the interface functions of the general processing module are more integrated and more required. In this paper a way of hardware function subareas is adopted to realize the integration and modularization of a general processing module in an aviation display and control system, and the configuration of FPGA and application software is used to realize the system's different requirements so as to realize the detection and isolation of module's error. Through system simulation tests and flight tests it is verified that the general processing module can meet the demands of the system. Moreover, the module helps reduce the system's size, weight, and power consumption, and increases its reliability.