Thus, an approach of Flight Control Law (FCL) model design and application for aircraft conceptual design is researched.
为此，本文进行了飞机总体设计中的飞行控制律模型设计与应用方法研究。
From the parameter identification theory, an aircraft sizing method is put forward in the aircraft conceptual design phase.
提出一种在飞机概念设计中基于参数辨识理论的设计参数分析方法。
Simulation result indicates that the equivalent moment derivatives model can be used in the evaluation of aircraft conceptual design and flight control system design.
验证表明，等效力矩导数模型可用于评估设计方案或指导飞行控制系统设计。
In mission definition stage, conceptual design phase and preliminary design phase, multidisciplinary optimization is especially significant for improving integration performance of aircraft.
在飞机设计各阶段中，任务定义阶段、概念设计阶段和初步设计阶段的综合优化设计对提高飞机整体性能具有极其重要的意义。
The quality and efficiency of conceptual aircraft design are improved.
从而提高飞机总体设计的质量和效率。
The work present here is the designing and evaluating techniques of Flight Control Law (FCL) from the point of view of conceptual aircraft design.
本文从总体设计的角度，对飞控系统控制律设计与评估方法进行了初步的探讨。
The work present here is the designing and evaluating techniques of Flight Control Law (FCL) from the point of view of conceptual aircraft design.
本文从总体设计的角度，对飞控系统控制律设计与评估方法进行了初步的探讨。
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