Challenge

Project 2 - Implement the Code for controlling the retraction and extension of Airplane’s landing gear

Actually an airplane has 3 gears for landing :

•

Nose Gear

•

Left Gear

•

Right Gear

There is a hydraulic pump which is exerting pressure to the

gears to bring it down or pull it up and that pump is

electrically driven.

Every leg of the gear has one limit switch

.Nose gear has

one extra Squat Switch to determine whether the airplane

is in ground or not.

Switch State

State of Gears

Limit Switch CLOSED

Gear is UP

Limit Switch OPENED

Gear is DOWN

Switch State

State of Airplane

Squat Switch CLOSED

Airplane is grounded and Gears

are locked

Squat Switch OPENED

Airplane is taking off / landing /

airborne

A direction valve is controlled by the software to allow the

hydraulic pressure to either raise or lower the landing gear

Status of Direction Valve

States of landing gear

Direction valve = Down

(Gear Down)(Parked at bay or Landed)

Direction valve = Up

Raising Gear(Taking Off)

Control of hydraulic pump for the

landing gear part is disabled

Gear Up(Airborne)

Direction valve = down

Lowering Gear(Landing)

Input for the Direction Valve

Pilot’s Lever State

Direction Valve State

Lever UP

Direction valve = Up

Lever Down

Direction valve = Down

Pilot’s Lever State

Light Status

Lever Rising Edge

Red

Lever Falling Edge

Every gear has one light. According to the state of the

gear,color of light is changing

Landing Gear State

Light Status

Gear is up

OFF

Gear is down

Green

Gear in transit(Raising or

Lowering)

Red

There is a possibility that the plane is about to take off and

an emergency comes where pilot has to abort the take off

•

When taking off,to ensure that its right time to raising the

gear,check for at least 4 seconds that squat switch is open

When the airplane is parked at the bay and nose gear is

down,then the nose gear is always experiencing a pressure

on it due to airplane weight,weight of luggage and weight

of passengers boarding on the airplane.Hydraulic

mechanism is monitoring the pressure exerted on the

nose gear and to neutralize that pressure its applying a

pressure on the opposite direction

Hydraulic Control can detect the rising edge and falling

edge of pilot’s lever

•

In case of Hydraulic system failure,there are two gas

pressurized springs by which gears can be extended

•

The case of failure of Squat Switch is ignored

Checking

before

Take off

Delay 3s

Gear

Down

Raising

Gear

Checking

before

Landing

Lowering

Gear

Pilot’s Lever Rising && Squat Switch

Open / Lights = Green

Squat Switch Close or Pilot’s Lever falling/

Lights = RED

Pilot’s Lever UP / Direction Valve = UP,

Lights = RED

Gear UP

Limit Switch Closed /

Lights OFF, Control for

landing gear disabled

Pilot’s Lever falling / Control enabled

,Lights = Red

Pilot’s Lever Down/ Direction Valve = DOWN

Pilot’s Lever Raising / Lights = RED

Pilot’s Lever Falling/ Lights = RED

Limit Switch Opened/

Lights = Green

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