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基于飞行性能最优的多操纵面飞机配平研究
引用本文:刘艳,高正红. 基于飞行性能最优的多操纵面飞机配平研究[J]. 飞行力学, 2009, 27(5)
作者姓名:刘艳  高正红
作者单位:西北工业大学翼型叶栅空气动力学国家级重点实验室;
摘    要:
从飞行性能最优的角度,对多操纵面飞机的配平原则与算法进行了研究。以瑞典FO I开发的ADM IRE为例,根据所建立的配平原则与算法对其进行了重新配平。比较了新配平方法与原配平方法的飞行性能,结果证实采用新配平方法的飞机飞行性能较好,说明所建立的配平原则与方法是合理的。

关 键 词:多操纵面  配平  飞行性能  控制分配  

Trimming for Aircraft with Multiple Control Effectors Based on Flight Performance Optimization
LIU Yan,GAO Zheng-hong. Trimming for Aircraft with Multiple Control Effectors Based on Flight Performance Optimization[J]. Flight Dynamics, 2009, 27(5)
Authors:LIU Yan  GAO Zheng-hong
Affiliation:National Key Laboratory of Aerodynamic Design and Research;NWPU;Xi'an 710072;China
Abstract:
On the aspect of getting the optimal flight performance,this paper discusses the trimming principle and solution for the aircraft with multiple control effectors.The Aero-Data Model in Research Environment(ADMIRE) developed by FOI was trimmed based on the principle and solution developed in this paper.The ADMIRE using the new trimming solution was compared with the original one.The results indicate that the ADMIRE using the new trimming solution has better flight performance,which means the principle and so...
Keywords:multiple control effectors  trimming  flight performance  control allocation  
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