Research Article
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.
|