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作业成本计算法是以作业为基础的成本核算方法,它建立在“作业消耗资源,产品消耗作业”两个前提下,是一种比较准确的成本计算方法。在作业成本法的基本原理的基础上,设计出了作业成本的计算流程,并结合矩阵理论建立了作业成本计算的数学模型。 相似文献
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对指派问题匈牙利解法的两点改进 总被引:2,自引:0,他引:2
张联朋 《西安航空技术高等专科学校学报》2007,25(1):64-66
提出了利用独立0元素在矩阵中的特殊位置来寻找独立0元素的方法,并对盖0线的画法做了重要改进。 相似文献
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Thomas S. Richardson Cormac McFarlane Askin Isikveren Ken Badcock Andrea Da Ronch 《Progress in Aerospace Sciences》2011,47(8):647-659
One of the main drivers behind the SimSAC project and the CEASIOM software is to bring stability analysis and control system design earlier into the aircraft conceptual design process. Within this paper two very different aircraft are considered, a conventional T-tail based on the existing EA500 Very Light Jet and the second, a novel Z-wing configuration known as the GAV or general aviation vehicle. The first aircraft serves as a baseline comparison for the second, and the cruise case is considered as a benchmark for identifying potential drag reductions and aircraft stability characteristics. CEASIOM, the Computerised Environment for Aircraft Synthesis and Integrated Optimisation Methods, is used to generate aerodynamic data sets for both aircraft, create trim conditions and the associated linear models for classical stability analysis. The open-loop Z-wing configuration is shown to display both highly unstable and coupled modes before a multivariable Stability Augmentation System (SAS) is applied both to decouple and stabilise the aircraft. Within this paper, these two aircraft provide a test case with which to demonstrate the capabilities of the CEASIOM environment and the tools which have been developed during the SimSAC project. This new software suite is shown to allow conceptual development of unconventional novel configurations from mass properties through adaptive-fidelity aerodynamics to linear analysis and control system design. 相似文献
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