Investigation on the Horizontal Landing Velocity and Pitch Angle Impact on the Soft-Landing Dynamic Characteristics

Table 16

Impact on the maximum force of secondary struts under typical lunar inclination conditions.

Lunar inclination (°)	Secondary struts 1/2 max force (N)	Error	Note
0		/	/
6 ()		-41.5%/57.7%	The secondary strut 1 has the least force
27.7 ()		3.7%/153%	Both secondary struts 1 and 2 have the maximum force