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飞控系统风洞虚拟飞行试验评估指标与评估要求
引用本文:黄敏,王中伟,郭振云,钮耀斌.飞控系统风洞虚拟飞行试验评估指标与评估要求[J].国防科技大学学报,2017,39(4):144-148.
作者姓名:黄敏  王中伟  郭振云  钮耀斌
作者单位:国防科学技术大学 航天科学与工程学院,国防科学技术大学 航天科学与工程学院,国防科学技术大学 航天科学与工程学院,国防科学技术大学 航天科学与工程学院
基金项目:国家自然科学基金项目(No. 51505487),国防科技大学科研计划项目(No. JC15-01-02)
摘    要:为明确风洞虚拟飞行试验能够评估的飞控系统性能,并为风洞虚拟飞行试验评估方法设计做出铺垫,针对风洞虚拟飞行试验特点,提出了风洞虚拟飞行试验能够评估的飞行性能指标及飞行品质指标,比较了风洞虚拟飞行试验与半实物仿真和飞行试验的评估能力差异;仿真分析了风洞虚拟飞行试验特点会造成的风洞虚拟飞行试验与自由飞行的评估结果差异;从试验、数据处理、性能评定等方面,提出了评估这些指标对风洞虚拟飞行试验评估方法的具体要求,并比较了它与半实物仿真和飞行试验的评估要求差异。

关 键 词:飞行控制系统评估  风洞虚拟飞行试验  评估指标  评估方法  半实物仿真  飞行试验
收稿时间:2016/4/20 0:00:00
修稿时间:2016/7/31 0:00:00

Analysis of the evaluation indexes and requirements of the wind tunnel based virtual flight testing for flight control systems
HUANG Min,WANG Zhongwei,GUO Zhenyun and NIU Yaobin.Analysis of the evaluation indexes and requirements of the wind tunnel based virtual flight testing for flight control systems[J].Journal of National University of Defense Technology,2017,39(4):144-148.
Authors:HUANG Min  WANG Zhongwei  GUO Zhenyun and NIU Yaobin
Institution:College of Aerospace Science and Engineering, National University of Defense Technology, Changsha 410073, China,College of Aerospace Science and Engineering, National University of Defense Technology, Changsha 410073, China,College of Aerospace Science and Engineering, National University of Defense Technology, Changsha 410073, China and College of Aerospace Science and Engineering, National University of Defense Technology, Changsha 410073, China
Abstract:In order to determine the flight control system (FCS) performances which the wind tunnel based virtual flight testing (VFT) can evaluate, and lay the foundations for designing the VFT evaluation methods, the evaluation indexes of VFT and the requirements of VFT evaluation methods for FCSs were analyzed. Firstly, according to the features of VFT, the flight performance indexes and flight quality indexes of FCSs which VFT can evaluate were proposed, and the evaluation capability differences among the VFT, hardware-in-the-loop simulation (HILS), and flight tests were compared. Then, the differences of evaluation results between VFT and free-flight caused by the features of VFT were compared. Lastly, from the aspects of testing, data processing, and the performance determination, the specific requirements of the VFT evaluation methods for evaluating the above indexes were proposed. And the evaluation requirement differences among the VFT, hardware-in-the-loop simulation (HILS), and flight tests were compared.
Keywords:flight control system evaluation  wind tunnel based virtual flight testing  evaluation indexes  evaluation methods  hardware-in-the-loop simulation  flight tests
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