PDF(208 KB)
PDF(208 KB)
PDF(208 KB)
单星修正惯导系统初始定位定向误差原理
Principle of Correcting the Initial Positioning and Orientating Errors ofInertial Guidance System by Single Star
| {{custom_ref.label}} |
{{custom_citation.content}}
{{custom_citation.annotation}}
|
/
| 〈 |
|
〉 |