Claims

Claim for managing body axis system using fibre optics

An equipment comprising step of :

power on ethernet with a Li-Fi routing capabilities and

emitter could be a photodiode or laser or LED and

emitter without analog power supply control and

emitter having photonic capability(for e.g halogens ) and

ip that carries light to trigger analyzers and

ip that could receive photons from a centralized emission where ip transmits photons from anywhere on earth in case of power failure and

the co-efficients of x-axis of aircraft like the series within the realtime bar chart of analyzers whose power is controlled by POE(emitter) clearly showing the pressure on aerodynamic centre which varies as per angle of attack and fuselage variables(for e.g cargos weight,fuel readings,engine analytics,propeller analytics,thrust analytics,regression analytics and drag analytics) as per yawing moment which may be positive or negative and its repurcursions of these x-axis coefficients on the co-efficients of y-axis and z-axis and

the coefficients of y-axis of aircraft like the series within the realtime bar chart of analyzers whose power is controlled by POE(emitter) which varies as per the rolling moment,positive as well as negative coefficients and its repurcursions of these y-axis co-efficients on the co-efficients of x-axis and z-axis mentioned above and

the coefficients of z-axis of aircraft like the series within the realtime bar chart of analyzers whose power is controlled by POE(emitter) which varies as per the lift as well as the limits that control stall moment of aircraft and its repurcursions of these z-axis co-efficients on the co-officients of x-axis and y-axis which controls pitching moment

will be provided

Claim for managing earth axis system using fibre optics
An equipment comprising step of :
the co-efficients of x-axis of aircraft like the series within the realtime bar chart of analyzers whose power is controlled by POE(emitter) clearly showing the pressure on aerodynamic centre which varies as per angle of attack and fuselage variables(for e.g cargos weight,fuel readings,engine analytics,propeller analytics,thrust analytics,regression analytics and drag analytics) and its repurcursions of these x-axis coefficients on the co-efficients of y-axis and z-axis and

the coefficients of y-axis of aircraft like the series within the realtime bar chart of analyzers whose power is controlled by POE(emitter) which varies as per the yawing moment,positive as well as negative coefficients and its repurcursions of these y-axis co-efficients on the co-efficients of x-axis and z-axis mentioned above and

the coefficients of z-axis of aircraft like the series within the realtime bar chart of analyzers whose power is controlled by POE(emitter) which varies as per the lift as well as the limits that control stall moment of aircraft and its repurcursions of these z-axis co-efficients on the co-officients of x-axis and y-axis

the co-efficients of x-axis stored in realtime serialized persistence object and
the co-efficient of centre of gravity of aircraft and co-efficent of earths axis which would also be part of
the co-officients of x-axis and would be stored in serialized persistence object which would be driven by the
light transmissions from the emitter that control all the co-efficents of x-axis where the ratio of bar chart coefficent of centre of gravity is always the same as the bar chart co-efficents of earths axis as well as co-efficients of x-axis of body axis and

the co-efficients of y-axis stored in realtime serialized persistence object and
the co-efficient of centre of gravity of aircraft and co-efficent of earths axis which would also be part of
the co-officients of y-axis and would be stored in serialized persistence object which would be driven by the
light transmissions from the emitter that control all the co-efficents of y-axis where the ratio of bar chart coefficent of centre of gravity is always the same as the bar chart co-efficents of earths axis as well as co-efficients y-axis of body axis and

the co-efficients of z-axis stored in realtime serialized persistence object and
the co-efficient of centre of gravity of aircraft and co-efficent of earths axis which would also be part of
the co-officients of z-axis and would be stored in serialized persistence object which would be driven by the
light transmissions from the emitter that control all the co-efficents of z-axis where ratio of the bar chart coefficent of centre of gravity is always the same as the bar chart co-efficents of earths axis as well as co-efficients z-axis of body axis

Claim for managing stability axis system using fibre optics
An equipment comprising step of :
the co-efficients of x-axis of aircraft like the series within the realtime bar chart of analyzers whose power is controlled by POE(emitter) clearly showing the pressure on aerodynamic centre which varies as per angle of attack and fuselage variables(for e.g cargos weight,fuel readings,engine analytics,propeller analytics,thrust analytics,regression analytics and drag analytics) and its repurcursions of these x-axis coefficients on the co-efficients of y-axis and z-axis and

the co-efficients of x-axis stored in realtime persistent object having a series of bar chart like the thrust and drag force where propeller analytics showing the co-efficients of thrust and drag on the analyzer controlled by the light emitter depending on angle of attack

the co-efficients of z-axis stored in realtime serialized persistence object and
the co-efficient of centre of gravity of aircraft and z-axis co-efficient of body axis would be stored in serialized persistence object which would be driven by the light transmissions from the emitter that control all the co-efficents of z-axis on body axis where ratio of the bar chart coefficent of centre of gravity is always the same as the bar chart z-axis co-efficients of body axis

the co-efficients of z-axis stored in realtime persistent object having a series of bar chart like the lift and stall moment where centre of gravity analytics showing the co-efficients of lift and stall moment shown on the analyzer controlled by the light emitter depending on angle of attack

Claim for transforming earth axis to body axis using fibre optics
An equipment comprising step of :

a horizontal plane which is the complete aircraft travel path  is the set co-officients on y-axis of bar chart which is the altitude at which the aircraft is travelling stored in serialized persistent object and

a yaw co-efficient is the series of co-efficients on x-axis on bar chart whose values are nothing but ratio of earth axis system variables like x  axis co-oefficients of body axis system stored in the realtime serialized persistent object vs the co-efficients on the horizontal plane on the y-axis on bar chart which would always be the same on the analyzer whose x and y values are retrieved from realtime serialized persistent object and

a pitch co-efficient is the series of co-efficients on x-axis of bar chart whose values are nothing but ratio of earth axis system variables like the z-axis co-effiecients in the body axis system stored in the realtime serialized persistent object vs the co-efficients on the horizontal plane on the y-axis of bar chart which would always be the same on the analyzer whose x and y values are retrieved from realtime serialized persistent object

a roll co-efficient is the series of co-efficients on x-axis of bar chart whose values are nothing but ratio of earth axis system variables like the y-axis co-effiecients in the body axis system stored in the realtime serialized persistent object vs the co-efficients on the horizontal plane on the y-axis of bar chart which would always be the same on the analyzer whose x and y values are retrieved from realtime serialized persistent object

will be provided

Claim for transforming stability axis to body axis using fibre optics
An equipment comprising step of :
the co-efficients of y-axis on the bar chart are the positive and negative values of angle of attack and

the lateral stability transform coefficient is the series of co-efficients of x-axis on the bar chart are the ratio of body axis  x-axis co-efficients variables stored in the realtime serialized persistence object vs the co-efficients of angle of attack on the y-axis of bar chart which would always be the same on the analyzer whose x and y values are retrieved from realtime serialized persistence object and

the longitudinal stability transform coefficient is the series of co-efficients of x-axis on the bar chart are the ratio of body axis z-axis co-efficents stored in the realtime serialized persistence object vs the co-efficients of angle of attack on the y-axis of bar chart which would always be the same on the analyzer whose x and y values are retrieved from realtime serialized persistence object

will be provided

Claim for aircraftposition analytics process

A process which comprising step of :

a method that operates at realtime and

a method that updates all the use cases for e.g roll,yaw,pitch,stall,lift and other fuselage coefficient and

on each updation current x,y,z axis per process gets updated and

aircraft stability co-efficient which is the average of all x-axis ,y-axis and z-axis coefficients of all use cases and

aircraft stability gradient is the aircraft stability divided by 100 and

stability failure is updated where the failure process and its transaction id is recorded

will be provided

Claim for end of day 

A process comprising step of  :

update EarthAxisSystem and
update StabilityAxisSystem and
update BodyAxisSystem
update EarthToBodyAxisTransform
update BodyAxisToRoll

update BodyAxisToPitch
update BodyAxisToYaw
update StabilityToBodyAxisTransform
update StabilityToLift
update StabilityToStall
update StabilityToDrag
update EarthToDrag
update StabilityToFuel
update EarthToFuel
update StabilityToAngleOfAttack
update EarthToAngleOfAttack
update StabilityToCargo
update EarthToCargo
update StabilityToCentreOfGravity
update EarthToCentreOfGravity
update StabilityToEngine
update EarthToEngine
update StabilityToPressure
update EarthToPressure
update StabilityToPropeller
update EarthToPropeller
update EarthToRegression
update StabilityToRegeression
update EarthToThrust
update StabilityToThrust
insert into into AngleOfAttackEarth Analyzer
insert into AngleOfAttackStabilty Analyzer
insert into CargoEarth Analyzer
insert into CargoStability Analyzer
insert into CentreOfGravityEarth Analyzer
insert into CentreOfGravityStability Analyzer
insert into DragEarth Analyzer
insert into DragStability Analyzer
insert into EngineEarth Analyzer
insert into EngineStability Analyzer
insert into FuelEarth Analyzer
insert into FuelStability Analyzer
insert into LiftStability Analyzer
insert into PitchEarth Analyzer
insert into PressureEarth Analyzer
insert into PressureStability Analyzer
insert into PropellerEarth Analyzer
insert into PropellerStability Analyzer
insert into RegressionEarth Analyzer
insert into RegressionStability Analyzer
insert into RollEarth Analyzer
insert into StallStability Analyzer
insert into ThrustEarth Analyzer
insert into ThrustStability Analyzer
insert into YawEarth Analyzer

truncate analyzers data

update at realtime speed and

update each process on aircraft position analytics object and

update all analyzers and

trucate data from bodyaxissystem,earthaxissystem,stabilityaxissystem as well as transformations data is truncated

Claim for objects within the system

A framework consisting steps of :

a object that follows use case specific model and

a object where each process is containerised and has a factory(for e.g connections,persistence,jpa queries and security) per process

will be provided

Claim for aircraft drag using fibre optics

Claim for aircraft lift using fibre optics

Claim for thrust of aircraft using fibre optics
Claim for Wing Design using fibre optics

Claim for Tail Design using fibre optics

Claim for Fuselage Design using fibre optics

Claim for Propulsion Design using fibre optics

Claim for Landing Gear Design using Fibre Optics

Claim for Control Surfaces of Aircraft using Fibre Optics

Claim for compressible flow using fibre optics

Claim for incompressible flow using fibre optics

Claim for subsonic flow using fibre optics

Claim for transsonic flow using fibre optics

Claim for root locus using fibre optics

Claim for static stability of aircraft using fibre optics

Claim for Classical Feedback Control using fibre optics

Claim for Aileron Design using Fibre Optics

Claim for Elevator Design using Fibre Optics

Claim for Rudder Design using Fibre Optics

Claim for Aerodynamic Balance and Mass Balance using Fibre Optics

Claim for dynamic stability of aircraft using fibre optics

Claim for Virtual Work of aircraft using fibre optics

Claim for Energy Methods of aircraft using fibre optics

Claim for Matrix Methods of aircraft using fibre optics

Claim of bending of thin plates using fibre optics

Claim of structural vibration using fibre optics

Claim for Airworthiness of aircraft using fibre optics

Claim for Airframe load using fibre optics

Claim for buckling using fibre optics

Claim for Aircraft performance using fibre optics

Claim for Fatigue using fibre optics

Claim for Elasticity of Aircarft using fibre optics