equatorial orbit

基本解釋

All geostationary satellites orbit the earth in the equatorial plane at a height of 35,785 km above the equator and stand still at a fixed azimuth and altitude for an observer on the earth surface.
所有的地球同步衛(wèi)星都在赤道上空35，785 km高度運(yùn)行，相對(duì)於地麪觀測(cè)者來(lái)說(shuō)，它們的方位角和高度角是始終不變的。
Lagranges method is employed to derive the equations of motion for the system when the satellite is restricted to an orbit plane(such as the equatorial plane) and moves at a uniform angular velocity.
利用拉格朗日方法導(dǎo)出母星被限制在赤道麪上以均勻角速度運(yùn)動(dòng)時(shí)系統(tǒng)的動(dòng)力學(xué)方程。