Design and Test of Dual Actuator Nose Wheel Steering System for Large Civil Aircraft

Table 1

Optimal design results.

Parameter name	Value
/Nm	7000
/°	80
/°	20
/MPa	16.55
/MPa	0.55
/mm	88
/mm	64
/mm	16
/mm	200
/mm	153
/deg	44
/deg	64
	4
/	64390
	114720
	45.23%
	33.76%

is nose gear strut cylinder diameter.