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

Table 15

Impact on the maximum force of the primary strut under typical lunar inclination conditions.

Lunar inclination (°)	Primary struts 1/2 max force (N)	Error	Note
0		/	The primary strut 1 has the greatest force
12 ()		-2.7%/25.6%	The primary strut 1 has the greatest force
27.7 ()		-7.6%/-7.7%	Both primary struts 1 and 2 have the least force