常見例句Abstract: All orbits by which targets can be covered are described according to the longitude of ascending node. 文摘:以陞交點(diǎn)經(jīng)度的範(fàn)圍來描述所有能覆蓋到目標(biāo)的軌道。All orbits by which targets can be covered are described according to the longitude of ascending node. 以陞交點(diǎn)經(jīng)度的範(fàn)圍來描述所有能覆蓋到目標(biāo)的軌道。Determining the attainability domain of aeroassisted orbital plane change, i.e. the inclination and the longitude of the ascending node, is a very important problem. 航天器進(jìn)行氣動(dòng)力輔助異麪變軌時(shí)，確定可達(dá)範(fàn)圍(變軌結(jié)束時(shí)的傾角和陞交點(diǎn)赤經(jīng))是一個(gè)十分重要的問題。right ascension of satellite ascending node 衛(wèi)星陞交點(diǎn)赤經(jīng)ascending node of satellite orbit 衛(wèi)星軌道陞交點(diǎn)METHOD FOR ORBIT DESIGN USING LONGITUDE OF ASCENDING NODE 利用陞交點(diǎn)經(jīng)度進(jìn)行軌道設(shè)計(jì)的方法 返回 ascending node