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小型无人机平尾优化设计
引用本文:安佳宁,陈小昆.小型无人机平尾优化设计[J].宇航计测技术,2013,33(4):62.
作者姓名:安佳宁  陈小昆
作者单位:1、中国人民解放军92419部队,辽宁 125106;; 2、中国人民解放军96311部队,湖南 418400
摘    要:提出了一种小型无人机平尾多目标优化方法。在保证飞行品质的前提下,实现了平尾阻力和尾撑结构质量最小的优化目标。通过优化,无人机纵向静稳定性降低,纵向操纵性得到提高。该方法对小型无人机平尾设计具有一定借鉴意义。

关 键 词:无人机    平尾    优化设计

Optimization Design of Horizontal Stabilizer for Mini-UVA
AN Jia-ning,CHEN Xiao-kun.Optimization Design of Horizontal Stabilizer for Mini-UVA[J].Journal of Astronautic Metrology and Measurement,2013,33(4):62.
Authors:AN Jia-ning  CHEN Xiao-kun
Institution:1、92419 Unit of PLA, Liaoning 125106; 2、96311 Unit of PLA, Hunan 418400
Abstract:A multi-objective optimization method was advanced to make the drag and structure mass minimum of horizontal stabilizer based the precondition of meeting flying qualities. After the optimization,the longitudinal stability reduced,the longitudinal control performance increased. This method has referential meaning for the design of horizontal stabilizer for Mini-UVA.
Keywords:UVA                                                                                                                        Horizontal stabilizer                                                                                                                        Optimization design
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