Space: Science & Technology / 2021 / Article / Tab 5

Review Article

Orbit Design Elements of Chang’e 5 Mission

Table 5

Error analysis results of aim point for ascent module.

StatisticsRelative position error (m)Relative velocity error (m/s)
RadialTransverseNormalRadialTransverseNormal

38.1−50.85.10.10.00.0
681.76614.7964.71.70.91.2
Min−1148.2−5549.0−1321.3−3.6−1.9−1.2
Max1550.25543.21050.36.51.61.3