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Space: Science & Technology
/
2021
/
Article
/
Tab 7
Review Article
Orbit Design Elements of Chang’e 5 Mission
Table 7
Flight data of aim point error for ascent module.
Relative position (m)
Relative velocity (m/s)
Radial
Transverse
Normal
Radial
Transverse
Normal
Nominal
9351.511
50252.499
0
0.317
−12.296
0
Flight
9272.041
49507.546
−59.200
0.287
−12.169
0.141
Difference
−79.470
−744.953
−59.200
−0.030
0.127
0.141