首页> 外文会议>AIAA atmospheric flight mechanics conference >Aircraft Dynamic Modeling in Turbulence
【24h】

Aircraft Dynamic Modeling in Turbulence

机译:湍流中的飞机动力学建模

获取原文

摘要

A method for accurately identifying aircraft dynamic models in turbulence was developed and demonstrated. The method uses orthogonal optimized multisine excitation inputs and an analytic method for enhancing signal-to-noise ratio for dynamic modeling in various levels of turbulence. A turbulence metric was developed to accurately characterize the turbulence level using flight measurements. The modeling technique was demonstrated in simulation, then applied to a subscale twin-engine jet transport aircraft in flight. Comparisons of modeling results from repeated maneuvers in a variety of turbulence conditions were used to demonstrate the effectiveness of the approach.
机译:开发并演示了一种用于精确识别湍流中飞机动力学模型的方法。该方法使用正交优化的多正弦激励输入和一种分析方法,该方法可增强信噪比,以便在各种湍流水平下进行动态建模。开发了一种湍流度量标准,以使用飞行测量值准确表征湍流水平。仿真中演示了该建模技术,然后将其应用于飞行中的小型双引擎喷气运输机。通过在各种湍流条件下重复进行演算得到的建模结果进行了比较,以证明该方法的有效性。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号