论文标题
光泽的光泽轨道大约$ l_1 $和$ l_2 $ offodravitations Sun-Earth System
Halo Orbits around $L_1$ and $L_2$ in the Photogravitational Sun-Earth System with Oblateness
论文作者
论文摘要
已经研究了具有无污垢的光机限制的三个身体问题，以获取拉格朗日点周围的光环轨道$ l_1 $和$ l_2 $的太阳 - 地球系统，其中太阳被视为辐射，地球作为块状球。对应于$ l_1 $ $ l_1 $和$ l_2 $的第四和第五阶近似值的光环轨道，以图形显示太阳的实际底压和不同的辐射压力。左右$ L_1 $的光环轨道的时间段随着底漆的增加而降低，随着辐射压力的增加而增加。由于在$ l_2 $左右的轨道时期内的底压和辐射压力增加，因此观察到反向效应。还可以观察到，由于辐射压力和填料的增加，左右$ L_1 $左右的光环轨道向辐射源转移。但是，由于辐射的增加，阳光轨道左右向辐射源转移到辐射源，但随着底漆的增加而退出。
The Photogravitational Restricted Three Body Problem with oblateness has been studied to obtain halo orbits around the Lagrangian points $L_1$ and $L_2$ of the Sun-Earth system in which the Sun is taken as radiating and the Earth as an oblate spheroid. The halo orbits corresponding to fourth and fifth order approximations around $L_1$ and $L_2$ for actual oblateness of the Earth and for different radiation pressures for the Sun are displayed graphically. The time period of halo orbits around $L_1$ decreases with increase in oblateness and increases with increase in radiation pressure. A reverse effect is observed due to increase in oblateness and radiation pressure on time period of orbits around $L_2$. It is also observed that halo orbits around $L_1$ shifts towards the source of radiation due to increase in both radiation pressure and oblateness. However, halo orbits around $L_2$ shifts towards the source of radiation due to increase in radiation but recedes with increase in oblateness.
