LEADER 00891nam0 2200253 450 001 000026210 005 20090615115958.0 100 $a20090615d1996----km-y0itay50------ba 101 0 $aeng 102 $aUS 105 $ay-------001yy 200 1 $aMatlab$ethe language of technical computing$eapplication program interface guide version 5 210 $aNatick (Mass.)$cMathWorks$d1996 215 $aVI, (paginazione varia)$cill.$d23 cm 300 $aSul front.: computation, visualization, programming 500 10$aMatlab$959185 517 1 $aApplication program interface guide version 5. 610 1 $aMatlab 676 $a519.40285$v20$9Analisi numerica applicata. Elaborazione dei dati. Programmi. 801 0$aIT$bUNIPARTHENOPE$c20090615$gRICA$2UNIMARC 912 $a000026210 951 $cDSA$aM 519.40285/20$bM s.i.$d2009 996 $aMatlab$959185 997 $aUNIPARTHENOPE LEADER 02804oam 2200457zu 450 001 9910140945603321 005 20241212220021.0 010 $a9781424479610 010 $a1424479614 035 $a(CKB)2670000000053915 035 $a(SSID)ssj0000451979 035 $a(PQKBManifestationID)12163765 035 $a(PQKBTitleCode)TC0000451979 035 $a(PQKBWorkID)10463766 035 $a(PQKB)11712360 035 $a(NjHacI)992670000000053915 035 $a(EXLCZ)992670000000053915 100 $a20160829d2010 uy 101 0 $aeng 135 $aur||||||||||| 181 $ctxt 182 $cc 183 $acr 200 10$a2010 IEEE Autotestcon 210 31$a[Place of publication not identified]$cIEEE$d2010 215 $a1 online resource $cillustrations 300 $aBibliographic Level Mode of Issuance: Monograph 311 08$a9781424479603 311 08$a1424479606 330 $aDemonstrations of avionics system and subsystem diagnostic capability are performed before a system or subsystem is verified. This ordinarily happens during the system design and demonstration phase of a program. In the case of aircraft or ground vehicles, there are several subsystem demonstrations, followed by a single system-level event. By the time a system or subsystem is ready for a functional demonstration of its diagnostic capability, there is already significant programmatic inertia towards achieving the next programmatic or contractual milestone. There is typically not enough available manpower, time-on-system, or even funding to test every possible fault in a given system or subsystem. Indeed, testing only the "relevant" faults, which the system's diagnostics have been built to address, can be a hugely time-consuming effort. Due to these constraints, diagnostic demonstrations are sometimes not conducted in a scientifically robust manner. Sometimes, certain testing techniques are used in an effort to expedite testing. These techniques include: emulating hardware faults and their detection circuitry in software, selecting only those faults which are easy to test or guaranteed to work, and choosing faults which do not significantly stress the diagnostics system. This paper describes a survey of diagnostic program managers in an attempt to characterize, and suggest remedies for, the time and budget-constrained fashion in which avionics diagnostics systems are functionally demonstrated today. 606 $aAutomatic test equipment$vCongresses 606 $aTesting$xData processing$vCongresses 615 0$aAutomatic test equipment 615 0$aTesting$xData processing 676 $a620.0044 702 $aieee 801 0$bPQKB 906 $aPROCEEDING 912 $a9910140945603321 996 $a2010 IEEE Autotestcon$92545511 997 $aUNINA