Any appropriate structural maintenance plan, based on a Safe-Life or a Damage Tolerance concept, is in close relation with the accuracy of in-service loads identification. The development of multichannel devices with integrated capabilities for in-flight preprocessing allows to get in-service data and flight results about any critical part of the equipped aircraft, but with sometimes such an amount of computations that the should-be simple in flight processing has to be transferred toward a ground facility.
Aircraft Tracking Optimization of Parameters Selection
1991
12 pages
Report
Keine Angabe
Englisch
Aircraft , Logistics Military Facilities & Supplies , Fighter aircraft , Structural response , Fatigue(Mechanics) , Accuracy , Damage , Maintenance , Multichannel , Preprocessing , Processing , Fatigue life , Tolerances(Mechanics) , Damage assessment , Stress analysis , Loads(Forces) , Airframes , Reprints , Failure(Mechanics) , Management , Foreign technology , Aircraft maintenance , Structural integrity , Allowable stress , MIRAGE 2000 Aircraft
Detection Threshold Selection for Tracking Performance Optimization
Online Contents | 1994
|Europäisches Patentamt | 2018
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