以编队卫星周期性相对运动条件为约束条件，提出了一种与传统动力学法相反的、研究编队卫星相对动力学的新思想。

Utilizing the orbit constraint derived from the presented algebraic method, the innovational methodology which uses the converse idea comparing with the traditional method is presented.

youdao

以编队卫星周期性相对运动条件为约束条件，提出了一种与传统动力学法相反的、研究编队卫星相对动力学的新思想。

Utilizing the orbit constraint derived from the presented algebraic method, the innovational methodology which uses the converse idea comparing with the traditional method is presented.

youdao