With the increasing complexity of aircraft system, it is more difficult to analyze and design the supportability of equipment. Aiming at this problem, this paper designed an aircraft supportability evaluation system, which is based on DEA and other assessment algorithm. Firstly, this paper gives the system's functional components and establishes the assessment software process of aircraft supportability scheme. Then, the DEA model algorithm of the evaluation system is introduced in detail. Finally, the paper applies evaluation system to analyze different supportability schemes. Moreover, the optimal supportability scheme is obtained. © 2014 Springer-Verlag.
CITATION STYLE
Zhi, J., Dong, S., & Han, R. (2014). The design of the aircraft supportability evaluation system. In Lecture Notes in Electrical Engineering (Vol. 297 LNEE, pp. 499–505). Springer Verlag. https://doi.org/10.1007/978-3-642-54233-6_55
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