导航三角形的识别只需基于单一特征量的匹配就可完成。
The recognition for navigation triangle can only be carried out on the matching of single characteristics quantity.
最后，引入验证识别环节有效地解决观测三角形与匹配的导航三角形产生的冗余问题。
Finally, a verification identification is used to solve the redundancies of the observed star triangle and the mapped navigation star triangle.
本文采用球面三角形原理推导了导航定位误差与陀螺姿态误差的关系式。
The relation between the navigation errors and the attitude errors of gyro was derived by use of spherical triangle.
应用推荐