Considering the aircraft as particle and using minimal input data to analyze the agility and post stall dynamic boundaries of TVC/PSM aircraft, which based on the analysis of turn rate plot and energy information.

 
  • 以飛機為質(zhì)點(diǎn) ,考慮在最少輸入數據情況下 ,基于轉彎速率圖并從能量的角度計算和分析了 TVC/PSM飛機的過(guò)失速動(dòng)態(tài)邊界 ;
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