Planned aircraft path angle based re-in orbit designing method, involves determining aircraft path angle and aircraft path angle limit value, and performing tilt angle calculating process to design orbit. | |
ZHOU W WANG Y MA H CHEN H NIE Z LI | |
2018 | |
公开日期 | 2018-05-04 |
URL标识 | 查看原文 |
申请日期 | 2017-12-07 |
WOS记录号 | [DB:DC_IDENTIFIER_WOSID] |
内容类型 | 专利 |
URI标识 | http://www.corc.org.cn/handle/1471x/3265668 |
专题 | 大连理工大学 |
作者单位 | UNIV DALIAN TECHNOLOGY (UYDA-C |
推荐引用方式 GB/T 7714 | ZHOU W WANG Y MA H CHEN H NIE Z LI. Planned aircraft path angle based re-in orbit designing method, involves determining aircraft path angle and aircraft path angle limit value, and performing tilt angle calculating process to design orbit.. 2018-01-01. |
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