• K. UMA MAHESWARI
• K. MALLIKARJUNA REDDY

The reliability of aircraft electrical components directly affects the combat performance of the aircraft. But the reliability is determined by the design, processing, environmental factors, accidents and other factors. Environmental testing is to prove the reliability and processing. The current reliability testing methods cannot precisely evaluate the comprehensive reliability of Software-Intensive Complex Systems. In order to solve the problem, it is necessary to research the method of carrying out the software-hardware interdependent reliability test. In this thesis, we do research on Software-hardware interdependent fault mode of Software-Intensive Complex Systems by collecting and studying the faults occurred in practical filed use. Then we design the software-hardware testing profile by adding software test profile to the reliability test profile, and put forward the idea about designing the test environment of software-hardware testing, which constitute a whole plan of software-hardware testing. And then a case study is demonstrated, which testifies the validation of the technique.

Design Optimization, Complex Systems,reliability, reliability test,Developmental Testingand Manufacturing Testing

"RELIABILITY TESTING METHODOLOGIES AND DISCRETE APPROACH FOR INTENSIVE COMPLEX SYSTEMS", International Journal of Emerging Technologies and Innovative Research (www.jetir.org), ISSN:2349-5162, Vol.5, Issue 10, page no.425-431, October-2018, Available :http://www.jetir.org/papers/JETIR1810456.pdf

"RELIABILITY TESTING METHODOLOGIES AND DISCRETE APPROACH FOR INTENSIVE COMPLEX SYSTEMS", International Journal of Emerging Technologies and Innovative Research (www.jetir.org | UGC and issn Approved), ISSN:2349-5162, Vol.5, Issue 10, page no. pp425-431, October-2018, Available at : http://www.jetir.org/papers/JETIR1810456.pdf