Space: Science & Technology / 2021 / Article / Tab 2

Research Article

Guidance Navigation and Control for Chang’E-5 Powered Descent

Table 2

Chang’E-5 LAM GNC flight results for descent and landing.


Landing horizontal velocity (m/s)0.0085
Landing vertical velocity (m/s)1.99
Landing angular rate (°/s)0.03
Angle between axis and local up direction (°)0.2
Angle between axis and local south direction (°)0.02
Propellant mass used during descent (kg)1898