Abstract Based on Gauss perturbation equation, the variation equation of orbit elements under both J2 and atmosphere perturbation is derived.

 
  • 摘要 基于高斯攝動(dòng)方程,推導了衛星在同時(shí)考慮J2攝動(dòng)和大氣阻力攝動(dòng)情況下的軌道要素變化方程。
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