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

Table 11

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

Initial pitch angle	Max force on secondary strut 1/2 (N)	Error	Note
0°		/	Max force on secondary strut 1
20° ()		-3.7%/18.5%	/
6.87° (0.12)		-48.1%/63%	Max force on secondary strut 2