与现有一些结果相比,这里提出的方法计算简单,而且适用于一般共面椭圆轨道情况,并保证全局最优性。
Comparedwith the existing results, this method is simpler in computation and valid for the case of elliptical orbits with global optimality guaranteed.
与现有一些结果相比,这里提出的方法计算简单,而且适用于一般共面椭圆轨道情况,并保证全局最优性。
Comparedwith the existing results, this method is simpler in computation and valid for the case of elliptical orbits with global optimality guaranteed.
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