In order to eliminate the stable error of airspeed and altitude which is inherently generated by the existing core algorithm of total energy control system (TECS) in eqs.

 
  • 將偏差控制與基于飛機總能量控制的解耦理論結合在一起,實(shí)現了對飛行速度和飛行高度的無(wú)穩差控制。
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