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Issue:
Aerodynamic Modeling and Experiment for Simulation of Helicopter Maneuver Flight
Author(s):
LI Jianbo
,
GAO Zheng
Pages:
116
-
118
Year:
2003
Issue:
2
Journal:
ACTA AERONAUTICA ET ASTRONAUTICA SINICA
Keyword:
直升机
;
机动飞行
;
仿真模型
;
非定常气动特性
;
气动干扰
;
神经网络
;
Abstract:
建立了适用于直升机机动飞行仿真的动力学模型.为了提高模型的真实度,着重通过瞬态操纵实验研究建立了旋翼非定常气动模型;又通过旋翼/机身气动干扰试验研究,并运用神经网络技术建立了一种新的机身气动力模型.使用该仿真模型做出的UH-60A直升机仿真计算结果与飞行试验数据符合良好.
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