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

Table 10

Impact of typical working conditions of initial pitch angle on maximum force of primary strut.

Initial pitch angle	Primary strut 1/2 max force (N)	Error	Note
0°		/	/
20° ()		14%/-2.7%	Maximum force on primary strut 1
6.87° (0.12)		7.5%/10.8%	Maximum force on primary strut 2