Research on Embedded Atmospheric Measurement Method Based on Three-point Method

Heng Wang, Jiamei Zhao, Weihe Shen, Hai Jiang, Zhilong Zhang, Jintian Tang
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Abstract

The requirements of maneuverability, velocity and control ability of modern aircraft are getting higher and higher. Effectively controlling the aircraft when flying at a high attack angle can greatly improve the maneuverability of the aircraft and reduce the stall speed of the aircraft. Flush Air Data Sensing System can indirectly obtain the angle of attack, sideslip angle, and the change of the incoming flow speed which provides necessary parameters for the flight control of the aircraft and meets the parameter measurement requirements of the aircraft. The algorithm research on pressure model and model trimming was conducted based on the three-point method with good real-time performance and high accuracy after study of traditional pressure models. And a series of experiments were performed to modify the accuracy of the model. After experimental verification, the model can be used to calculate the attack angle, sideslip angle, and flow velocity in flight projects, which can provide certain parameters or basis for aircraft flight control.
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基于三点法的嵌入式大气测量方法研究
现代飞机对机动性、速度和控制能力的要求越来越高。在大攻角飞行时对飞机进行有效控制,可以大大提高飞机的机动性,降低飞机的失速速度。齐平气流数据传感系统可以间接获取飞行器的迎角、侧滑角和来流速度的变化,为飞行器的飞行控制提供必要的参数,满足飞行器的参数测量要求。在对传统压力模型进行研究的基础上,基于实时性好、精度高的三点法对压力模型和模型裁剪进行了算法研究。并进行了一系列的实验来修正模型的精度。经实验验证,该模型可用于计算飞行项目中的攻角、侧滑角和流速,为飞机飞行控制提供一定的参数或依据。
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