Based on relative motion equation of satellite state transferring, analytic solution of two-impulse orbit transfer of constellation is derived, which is analytic equation of impulse control variable.

 
  • 基于衛星相對運動(dòng)狀態(tài)轉移方程,推導出了星座雙脈沖式變軌的理論解,即所要施加的脈沖控制量的解析式;
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