AbstractFlush Air Data Sensing System (FADS) forms a mission critical sub system in future reentry veh'/> Inverse Flush Air Data System (FADS) for Real Time Simulations
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Inverse Flush Air Data System (FADS) for Real Time Simulations

机译:用于实时仿真的逆嵌入空气数据系统(FADS)

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AbstractFlush Air Data Sensing System (FADS) forms a mission critical sub system in future reentry vehicles. FADS makes use of surface pressure measurements from the nose cap of the vehicle for deriving the air data parameters of the vehicle such as angle of attack, angle of sideslip, Mach number, etc. These parameters find use in the flight control and guidance systems, and also assist in the overall mission management. The FADS under consideration in this paper makes use of nine pressure ports located in the nose cap of a technology demonstrator vehicle. In flight, the air data parameters are obtained from the FADS estimation algorithm using the pressure data at the nine pressure ports. But, these pressure data will not be available, for testing the FADS package during ground simulation. So, an inverse software to FADS which estimates the pressure data at the pressure ports for a given flight condition is developed. These pressure data at the nine ports will go as input to the FADS package during ground simulation. The software is run to generate the pressure data for the descent phase trajectory of the technology demonstrator. This data is used again to generate the air data parameters from FADS algorithm. The computed results from FADS algorithm match well with the trajectory data.]]>
机译:<![cdata [ <标题>抽象 ara id =“par1”>嵌入式空气数据传感系统(FADS)形成任务未来再入车辆的关键子系统。 FADS使用从车辆的鼻帽进行表面压力测量,用于导出车辆的空气数据参数,例如攻击角度,侧面线,马赫数等。这些参数在飞行控制和引导系统中可用,并协助整体任务管理。本文正在考虑的时代利用位于技术示范车辆的鼻盖中的九个压力口。在飞行中,使用九个压力端口处的压力数据从FADS估计算法获得空中数据参数。但是,这些压力数据将不可用,用于在地面仿真期间测试FADS包。因此,开发了一种逆软件,其估计用于给定飞行条件的压力端口处的压力数据。九个端口处的这些压力数据将在地面模拟期间作为FADS包的输入。运行该软件以生成技术演示器的下降相位轨迹的压力数据。该数据再次用于从FADS算法生成空中数据参数。来自FADS算法的计算结果与轨迹数据相匹配。 ]]>

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