![]() ![]() The results show that the minimum relation perturbation conditions can reduce the J 2 effect significantly when the orbital element differences are small enough, and they can become rules for the design of satellite formation flying. Download from TGP and password-protected sites. Finally, the minimum relation perturbation conditions are established in order to reduce the influence of the J 2 effect. Features: Download your choice of images, music, video or any other files from websites automatically. The relationship of relative orbital elements and J 2 effect is obtained through simulations. In addition, when J 2 perturbation is concerned, we also find that the semi-major axes of the leading and following satellites should not be the same exactly in order to decrease the J 2 effect. They are distortion and drifting, respectively. Secondly, on the basis of the analysis of J 2 effect on relative orbital configurations, we find out that J 2 effect can induce two kinds of changes of relative orbital configurations. ![]() These shapes can be lines, ellipses or distorted closed curves. Firstly, under the condition of non-perturbation, we obtain many shapes of relative orbital configurations when the semi-major axes of satellites are equal. ![]() Download this template using the above button. In this paper, the relative orbital configurations of satellites in formation flying with non-perturbation and J 2 perturbation are studied, and an orbital elements method is proposed to obtain the relative orbital configurations of satellites in formation. Download and install the most recent version of Extreme Picture Finder. ![]()
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