The trajectory tracking system of BTT missile was studied. The nonlinear acceleration guidance logic was used on the outer loop to accomplish guiding. The acceleration autopilot was used on the inner loop.

 
  • 研究了傾斜轉彎(BTT)導彈的航跡跟蹤系統;外回路采用非線(xiàn)性過(guò)載制導指令的方式進(jìn)行制導;內回路為過(guò)載自動(dòng)駕駛儀.
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