Source code for RCAIDE.Library.Components.Landing_Gear.Nose_Landing_Gear
# RCAIDE/Compoments/Landing_Gear/Nose_Landing_Gear.py
#
# Created: Nov 2024, M. Clarke
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# IMPORT
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# RCAIDE imports
from .Landing_Gear import Landing_Gear
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# Nose_Landing_Gear
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[docs]
class Nose_Landing_Gear(Landing_Gear):
"""
Nose landing gear component that provides directional control during ground operations
and supports a portion of the aircraft's forward weight.
Attributes
----------
tag : str
Unique identifier for the nose landing gear component, defaults to 'nose_gear'
tire_diameter : float
Diameter of the nose gear tires, defaults to 0
strut_length : float
Length of the nose gear strut assembly, defaults to 0
units : float
Number of nose landing gear units, typically 1, defaults to 0
wheels : float
Number of wheels per nose gear unit, defaults to 0
Notes
-----
The nose landing gear typically carries 10-20% of the aircraft weight and provides
steering capability during taxi, takeoff, and landing.
**Major Assumptions**
* Located on aircraft centerline
* Provides steering capability
* Designed for lower loads than main gear
**Definitions**
'Steering Angle'
Maximum deflection angle available for directional control
See Also
--------
RCAIDE.Library.Components.Landing_Gear.Landing_Gear
Base landing gear class
RCAIDE.Library.Components.Landing_Gear.Main_Landing_Gear
Main gear component that works in conjunction with nose gear
"""
def __defaults__(self):
"""
Sets default values for the nose landing gear attributes.
"""
self.tag = 'nose_gear'
self.tire_diameter = 0.
self.strut_length = 0.
self.units = 0. # number of nose landing gear
self.wheels = 0. # number of wheels on the nose landing gear