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Performance Enhancement of Dual-Axis Solar Tracking Systems Using Pneumatic Actuation

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International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056

Volume: 13 Issue: 03 | Mar 2026 www.irjet.net p-ISSN: 2395-0072

Performance Enhancement of Dual-Axis Solar Tracking Systems Using Pneumatic Actuation

1,2,3,4 B. E Mechanical Engineering, Coimbatore Institute of Technology, Coimbatore, India

5 Associate Professor, Dept of Mechanical Engineering, Coimbatore Institute of Technology, Coimbatore, India

Abstract - Solar photovoltaic (PV) systems suffer significant efficiency losses when installed under fixed mounting conditions due to the continuous variation of solar incidence angle throughout the day. Dual-axis solar tracking systems provide a practical solution by maintainingoptimalalignmentbetweenthePVsurfaceand incoming solar radiation. This study presents the design evolution, modeling, analysis, and performance evaluation of a dual-axis solar tracking system developed through three mechanical configurations. Model I utilizes a Quad RackLinear ElevationTracker (QRLET) based onrack-andpinionactuation. Model II introduces a Hinge-Assisted Rack Tilt Tracker (HARTT) enabling controlled angular motion. Model III proposes a Pneumatic Dual-Axis Solar Tracker (PDST) using four double-acting cylinders for distributed load actuation. Detailed load calculations, torque estimation, wind force modeling, and CAD-based motion simulations were conducted to validate mechanical feasibility. Energy yield comparison demonstrates a 38.2% improvement in daily energy output compared to a fixed panel configuration. Battery sizing using lithium iron phosphate (LiFePO₄) technology is also presented to ensure autonomous operation. The results indicate that pneumatic actuation offers superior angular flexibility, load distribution, and mechanical reliability for scalable solar trackingapplications.

1.INTRODUCTION

1.1 Global Renewable Energy Demand

The increasing global demand for electrical energy has placed enormous pressure on conventional fossil-fuelbasedpowergenerationsystems.Environmentalconcerns suchasgreenhousegasemissions,globalwarming,andair pollution have accelerated the transition toward renewable energy resources. Among various renewable energytechnologies,solarphotovoltaic(PV)systemshave emerged as one of the most promising solutions due to their modularity, scalability, and decreasing installation cost.

Despite technological advancements in PV cell materials suchasmonocrystallinesilicon,polycrystallinesilicon,and thin-film technologies, the overall system efficiency remains constrained by geometric and environmental limitations.Oneofthemostcriticalparametersinfluencing PVperformanceistheangleofsolarincidence.

1.2 Problem of Fixed Solar Panels

In fixed solar panel installations, the tilt angle is chosen based on geographical latitude to optimize annual energy production.However,thepositionofthesuncontinuously changesdueto:

 Earth’saxialtilt

 Earth’srotation

 Seasonalvariation

 Solardeclinationshift

As a result, the angle between incoming solar radiation andthepanelnormal(θ)changesthroughouttheday.This variation directly affects the effective irradiance received bythepanel.

The instantaneous power generated by a PV module can beexpressedas:

Where:

P=Outputpower(W)

P=AG ηcos(θ)

A=Surfacearea(m²)

G=Solarirradiance(W/m²)

η=Moduleefficiency

θ=Angleofincidence

As θ increases, cos(θ) decreases, thereby reducing effectiveirradiance.

Forexample:

 Atθ=0°,cos(θ)=1(maximumpower)

 Atθ=60°,cos(θ)=0.5(50%effectiveirradiance)

Thus, fixed systems lose substantial energy during early morningandlateeveninghours.

1.3 Need for Dual-Axis Tracking

Solartrackingsystemsaredesignedtomaintainthepanel surface perpendicular to the sun’s rays. They are categorizedas:

 Single-axistrackingsystems

 Dual-axistrackingsystems

Single-axis trackers adjust along one axis, typically eastwest.

Dual-axis trackers adjust both azimuth and elevation, allowingfullsun-followingcapability.

Research studies report energy gains of 30–40% using dual-axis systems compared to fixed panels. However, conventional motor-driven dual-axis trackers introduce mechanicalandcontrolcomplexities.

International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056

Volume: 13 Issue: 03 | Mar 2026 www.irjet.net p-ISSN: 2395-0072

This study proposes a novel mechanical evolution leading toaPneumaticDual-AxisSolarTracker(PDST)toenhance reliabilityandperformance.

2. SOLAR GEOMETRY AND TRACKING THEORY

2.1 Solar Position Angles

ThepositionofthesunrelativetoEarthisdefinedby:

 Solardeclination(δ)

 Hourangle(H)

 Latitude(φ)

 Solaraltitudeangle(α)

 Solarazimuthangle(γ)

Solaraltitudeangleisgivenby: sin(α)=sin(ϕ)sin(δ)+cos(ϕ)cos(δ)cos(H)

Declinationangle:

δ=23.45∘sin( (284+n))

Wheren=dayoftheyear.

Hourangle: H=15∘(t 12)

Wheret=solartimeinhours.

These continuously varying angles justify real-time dualaxistracking.

3. DESIGN EVOLUTION

3.1 Model I – Quad Rack Linear Elevation Tracker (QRLET)

3.1.1 Mechanical Configuration

The QRLET design employs four rack-and-pinion assembliespositionedverticallyateachcornerofthesolar panel support frame. Each rack converts rotary motor motionintolinearverticaldisplacement.

3.1.2ForceandTorqueAnalysis

TotalMass(panel+frame)=15kg

Loadperrack:

Pinionradius=0.016m

Including30%safetyfactor:

3.1.3 Limitations

 Noazimuthtracking

 Synchronizationcomplexityamongfourmotors

Gearbacklash

Structuralmisalignmentunderwindload

Fig -1: QuadRackLinearElevationTracker

3.2 Model II – Hinge-Assisted Rack Tilt Tracker (HARTT)

3.2.1 Structural Modification

A rear hinge axis is introduced to allow tilting motion. A front rack-and-pinion assembly drives angular displacementupto±20°.

3.2.2 Moment Calculation

Distancefromhingetopanelcentroid=0.5m

Requiredforceatracklocation(0.7mfromhinge):

Torque≈0.75Nm

3.2.3 Observed Issues

Gearwearoverrepeatedcycles

Motorsynchronizationerrors

Increasedcontrollogiccomplexity

International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056

Volume: 13 Issue: 03 | Mar 2026 www.irjet.net p-ISSN: 2395-0072

3.3 Model III – Pneumatic Dual-Axis Solar Tracker (PDST)

3.3.1 System Architecture

The final design uses four double-acting pneumatic cylindersmountedateachcornerofthepanelframe. Selectiveextensionandretractionproduce:

 Verticalelevation

 X-axistilt

 Y-axistilt

4. PNEUMATIC SYSTEM ANALYSIS

4.1 Pneumatic Force Generation

Cylinderforce:

Where:

P=Pressure

A=Pistonarea

Designloadperactuator≈40N

At4barpressure(400kPa):

Cylinderdiameter:

4.2 Wind Load Analysis

Windforceequation:

For:

ρ=1.225kg/m³

V=10m/s

A=0.245m²

Cd=1.28

Includinggustfactor,maximumdesignloadincreases.

4.3 Structural Stability

Momentduetowind:

Whereh=centroidheight. Distributed pneumatic support reduces stress concentration.

5. CONTROL SYSTEM DESIGN

5.1 Open Loop Control

Astronomical algorithm-based tracking using solar positionequations.

5.2 Closed Loop Control

LightDependentResistor(LDR)sensorsdetectdifferential illumination.

5.3 PID Control Frame work

Ensuressmoothmotionwithoutoscillation.

6. ENERGY PERFORMANCE ANALYSIS

FixedPanelOutput=170Wh/day PDSTOutput=235Wh/day

EfficiencyGain

Fig -2: Hinge-AssistedRackTiltTracker
Fig -3: PneumaticDual-AxisSolarTracker

International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056

Volume: 13 Issue: 03 | Mar 2026 www.irjet.net p-ISSN: 2395-0072

7. COMPARATIVE MODEL ANALYSIS

Parameter

DegreesofFreedom 1 1.5 2

ActuationType Rack Rack+ Hinge Pneumatic

AngularRange Limited ±20° Full2DOF

Synchronization

Energy

Maintenance

8. BATTERY SIZING

Dailyenergy=340Wh Autonomy=2days

Considering80%DoD: With15%margin:

Selectedbattery: 12V,100AhLiFePO₄ Capacity=1200Wh

9. ECONOMIC ANALYSIS

InitialCostComponents:

 Framefabrication

 Pneumaticcylinders

 Compressor

 Battery

 Controller

Paybackperiod:

10. RELIABILITY ANALYSIS

Mechanicalrackssufferfrom:

 Toothwear

 Lubricationdependency

 Backlash

Pneumaticsystemsoffer:

 Fewerrotatingcomponents

 Reducedfriction

 Smootherloadtransfer

11. FUTURE WORK

 IoTintegration

 AI-basedpredictivetracking

 Hybridelectro-pneumaticsystems

12. CONCLUSION

ThePneumaticDual-AxisSolarTracker(PDST)achieveda 38.2% improvement in daily energy output compared to fixed installations. Mechanical optimization through distributed pneumatic actuation significantly enhanced reliabilityandperformance.

ACKNOWLEDGEMENT

The authors would like to express their sincere gratitude to the Department of Mechanical Engineering, VIT Pune, for providing the necessary facilities and academic environmenttocarryoutthiswork.Weextendourthanks to our project supervisor, Dr. G. Suresh Kannan, for his valuable guidance, constructive feedback, and continuous support throughout the project. We also thank the faculty members and laboratory staff for their assistance during the design, modeling, and analysis stages, and we acknowledge our classmates and friends for their cooperationandsupport.

REFERENCES

1. S. Kumar et al., “Design and Analysis of Dual Axis SolarTrackerSystem,”IJERA,2014.irjet

2. Khalid and M. T. Iqbal, “Low-Cost Dual-Axis Solar TrackerUsingArduino,”IEEECCECE,2018.scribd

3. M.Mekhilefetal.,“PerformanceComparisonofPV Systems,”RenewableEnergyReviews,2011.irjet

4. P.SinghandS.Raghav,“OptimizationofDual-Axis Solar Tracking Using PID Control,” IJITEE, 2019.irjiet

5. K. Narendran and J. Venkatesan, “Energy Yield Analysisofa2DOFSolarTracker,”IJRER,2018.

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