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Development of a real-time transport performance optimization methodology

机译:实时运输性能优化方法的开发

摘要

The practical application of real-time performance optimization is addressed (using a wide-body transport simulation) based on real-time measurements and calculation of incremental drag from forced response maneuvers. Various controller combinations can be envisioned although this study used symmetric outboard aileron and stabilizer. The approach is based on navigation instrumentation and other measurements found on state-of-the-art transports. This information is used to calculate winds and angle of attack. Thrust is estimated from a representative engine model as a function of measured variables. The lift and drag equations are then used to calculate lift and drag coefficients. An expression for drag coefficient, which is a function of parasite drag, induced drag, and aileron drag, is solved from forced excitation response data. Estimates of the parasite drag, curvature of the aileron drag variation, and minimum drag aileron position are produced. Minimum drag is then obtained by repositioning the symmetric aileron. Simulation results are also presented which evaluate the affects of measurement bias and resolution.
机译:基于实时测量和来自强制响应演算的增量阻力的计算,解决了实时性能优化的实际应用(使用宽体运输模拟)。尽管本研究使用对称的舷外副翼和稳定器,但可以设想各种控制器的组合。该方法基于导航仪器和最新运输工具上的其他测量结果。该信息用于计算风和迎角。推力是根据代表的发动机模型估算出的测量变量的函数。然后,将升力和阻力方程式用于计算升力和阻力系数。从强制激励响应数据中求解了阻力系数的表达式,该系数是寄生阻力,感应阻力和副翼阻力的函数。产生寄生阻力,副翼阻力变化的曲率和最小副翼位置的估计。然后通过重新放置对称副翼获得最小阻力。还提供了仿真结果,用于评估测量偏差和分辨率的影响。

著录项

  • 作者

    Gilyard Glenn;

  • 作者单位
  • 年度 1996
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  • 原文格式 PDF
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