航空学报
航空學報
항공학보
ACTA AERONAUTICA ET ASTRONAUTICA SINICA
2010年
2期
277-284
,共8页
代京%张平%李行善%于劲松
代京%張平%李行善%于勁鬆
대경%장평%리행선%우경송
测试性设计%建模%面向对象的贝叶斯网络%交叉熵%不确定性分析
測試性設計%建模%麵嚮對象的貝葉斯網絡%交扠熵%不確定性分析
측시성설계%건모%면향대상적패협사망락%교차적%불학정성분석
design for testability%modeling%object oriented Bayesian networks%cross entropy%uncertainty analysis
针对航空机电系统测试性设计(DFT)需求,提出基于面向对象的贝叶斯网络(00BN)与状态一测试关联灵敏度指标的系统测试性建模与分析的新方法.该建模方法能清晰地刻画系统故障与测试间的关联程度,反映复杂系统的层次结构关系.基于信息论的交叉熵原理提出状态-测试关联灵敏度指标,并给出计算方法.该指标反映复杂机电系统测试中的不确定性影响,克服了基于香农熵的测点评判分析方法的缺点,结合测试性建模获得的模型信息进行推理计算,可用于测试性的定量分析.运用该综合分析方法对飞机燃油系统进行测试性建模与分析,结果表明所提出的方法与指标在航空机电系统DFT中具有实用性.
針對航空機電繫統測試性設計(DFT)需求,提齣基于麵嚮對象的貝葉斯網絡(00BN)與狀態一測試關聯靈敏度指標的繫統測試性建模與分析的新方法.該建模方法能清晰地刻畫繫統故障與測試間的關聯程度,反映複雜繫統的層次結構關繫.基于信息論的交扠熵原理提齣狀態-測試關聯靈敏度指標,併給齣計算方法.該指標反映複雜機電繫統測試中的不確定性影響,剋服瞭基于香農熵的測點評判分析方法的缺點,結閤測試性建模穫得的模型信息進行推理計算,可用于測試性的定量分析.運用該綜閤分析方法對飛機燃油繫統進行測試性建模與分析,結果錶明所提齣的方法與指標在航空機電繫統DFT中具有實用性.
침대항공궤전계통측시성설계(DFT)수구,제출기우면향대상적패협사망락(00BN)여상태일측시관련령민도지표적계통측시성건모여분석적신방법.해건모방법능청석지각화계통고장여측시간적관련정도,반영복잡계통적층차결구관계.기우신식론적교차적원리제출상태-측시관련령민도지표,병급출계산방법.해지표반영복잡궤전계통측시중적불학정성영향,극복료기우향농적적측점평판분석방법적결점,결합측시성건모획득적모형신식진행추리계산,가용우측시성적정량분석.운용해종합분석방법대비궤연유계통진행측시성건모여분석,결과표명소제출적방법여지표재항공궤전계통DFT중구유실용성.
In order to meet the demand of design for testability(DFT)for aviation electromechanical systems,a novel approach for system testability modeling and analysis is proposed which is based on object oriented Bayesian networks(OOBN) and the state-test association sensitivity index.The modeling approach can describe clearly the inter-dependent relationship between system faults and test symptoms,and reflect the hierarchical structure of complex systems.Based on the cross entropy principle in information theory,a novel index named state-test association sensitivity index is proposed together with its calculating methods.The index can reflect the impact of uncertainties in complex electromechanical system tests,and overcome the shortcomings of the test point analysis approach based on Shannon entropy.Combined with the testability model information,it can be used in quantitative testability analysis.The approach is used on an aircraft fuel system testability modeling and analysis,and the result shows the practicability of the proposed approach and index in aviation electromechanical system DFT.