normal design aircraft 中文意思是什麼
normal design aircraft
解釋
常規飛機-
The objective of this thesis is to design an artificial neural network adaptive reconfigurable flight control law basing on the view of engineering and to establish a flight simulation system with normal aircraft, fault aircraft, normal flight control law, reconfigurable flight control law and fault verification by c + + program
本文目的是從工程角度考慮，重點開發神經網路自適應的自修復重構飛行控制律。並在c + +環境下建立具有正常與故障飛機、正常與自修復重構飛行控制律和故障認定等模塊的飛行綜合模擬系統。 -
Using this model, not only the normal static and dynamic characters of aircraft epgs but also the fault state system can be simulated. it is useful to analyse and design aircraft epgs
利用本文開發的模型，不僅能模擬電源系統及其部件正常工作時的穩態和動態特性，而且能模擬其故障狀態，有助於對飛機電源系統進行分析和設計。 -
Following problems are mainly discussed in this work : how to build a parametrical finite element ( fe ) model how to choose the design parameters, constraints and objective of the correction model how to evaluate different sensitivity calculating methods and choose optimization algorithms how to get the normal mode - shapes and describe the relativity between normal mode - shapes how to solve the correction problem of fe model by using structure optimization techniques in each paragraph, illustrative examples are used to explain the methods and finally an engineering application of an aircraft correction is presented in the end
主要進行了如下幾個方面的工作：參數化有限元模型的建立；修正模型設計參數、約束及目標函數的確定；靈敏度方法的比較及優化演算法的選取；固有振型的獲取及模態相關性的定量描述；採用結構優化技術解決有限元模型修正問題。在模態修正過程中，由於修正固有振型涉及大量的有限元計算結果數據，此前，雖有不少文獻在理論上研究了它的修正方法，但都沒有給出工程應用實例，而本文解決了固有振型修正的工程應用問題。
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