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Hamilton
Construction UAV
Proposal
By: Malcolm Aranda
For: Michael Battaglino
Customer Bio
Hamilton Construction
• International construction company
• Involved in small to large housing developments
• Has branched off into nuclear power plant decommissioning
Unmanned Aerial Vehicle (UAV) Requirements
• two-hour endurance
• Vertical take-off and landing
• Operate day and night
• Easy to use software
Vehicle Design
• Medium sized quad-copter
• Propellers will need to be
protected
• Will need electro-optical and
infrared cameras
Propulsion System
• Hybrid gas and electric propulsion
• Gasoline engine powers a generator
• Power from generator gets stored into a battery and power distribution module.
• Propellers are powered through the electricity
(Skyfront, n.d.)
Battery
• Medium Capacity Lithium Ion battery
• Will provide a total of 4 min backup power
for emergency landing
• Weight: .5 lbs
• 10,000 mAh
Tenergy,n.d.
Propeller
• Eight inch propeller
• Safety Cage for protection
Hobby King, n.d.
Safelight, n.d.
Sensor Package
• Controp Micro-Stamp
• Three gimbal stabilized system
• Single LRU gyro-stabilized electro-optic system
• Uncooled IR with Dual FOV
• X4.8 continuous zoom day camera
• Low power consumption
• Very low weight
(Controp, n.d.)
Control Hardware
• Ruggedized tablet
• Touchscreen
• Preloaded software
• Internet connectivity
Software
• Easy to use
• Touchscreen tablet included
• Programmable autonomous flight plan
• Manual operation
• Autopilot
• Camera operated through touchscreen
Performance/Endurance
• Capable of 2.5 hours of flight
• Line of Sight connectivity
• 2.5 km range
Desired Launch and Recovery site
• Clear area that is 20 ft x 20 ft
• Will allow for any wind corrections and site familiarity
• Platform has fixed landing skids similar to helicopter
• Skids are made of 3D printed plastic
• Easy to repair/replace
Computer Aided Design (CAD)
Computer simulations will help determine :
• Performance needs
• Energy consumption
• Fuel burn
• Estimated noise output
• Aerodynamic properties
• Capabilities/limitations
Test and Evaluation (phase one)
• Conducted in rural area to ensure safety
• Validation of computer simulations
• Conduct take-off, landing, and endurance
• Limit altitude to max 20 ft.
• Gather data for follow on testing
Test and Evaluation (phase two)
• Conduct full test of sensor package
• Testing will be done at military urban training environment
• Testing will help improve software
Final Test/Customer Validation
• Flight over live construction site
• Flight will be no less than 2 hours
• Show take-off and landing
• Let stakeholders test the ease of use of the software
• Show resiliency to outside frequencies from construction site
• “inspect” building frame
• Last stage of development prior to final agreement and product delivery
Final Product Delivery Timeline
Design phase
• 3 months for product design and computer simulation
Manufacturing
• 1 month to order and fabricate parts
• 2 weeks to test part compatibility and assemble
Testing
1st phase – 1 week of flight testing
• 1 week to improve autopilot and flight profiles
2nd phase – 1 week of urban environment testing
• Test sensor and software usability
Final phase – Live customer test
• Full capability verificaiton
References

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Hamilton uav presentation, M. Aranda

  • 1. Hamilton Construction UAV Proposal By: Malcolm Aranda For: Michael Battaglino
  • 2. Customer Bio Hamilton Construction • International construction company • Involved in small to large housing developments • Has branched off into nuclear power plant decommissioning
  • 3. Unmanned Aerial Vehicle (UAV) Requirements • two-hour endurance • Vertical take-off and landing • Operate day and night • Easy to use software
  • 4. Vehicle Design • Medium sized quad-copter • Propellers will need to be protected • Will need electro-optical and infrared cameras
  • 5. Propulsion System • Hybrid gas and electric propulsion • Gasoline engine powers a generator • Power from generator gets stored into a battery and power distribution module. • Propellers are powered through the electricity (Skyfront, n.d.)
  • 6. Battery • Medium Capacity Lithium Ion battery • Will provide a total of 4 min backup power for emergency landing • Weight: .5 lbs • 10,000 mAh Tenergy,n.d.
  • 7. Propeller • Eight inch propeller • Safety Cage for protection Hobby King, n.d. Safelight, n.d.
  • 8. Sensor Package • Controp Micro-Stamp • Three gimbal stabilized system • Single LRU gyro-stabilized electro-optic system • Uncooled IR with Dual FOV • X4.8 continuous zoom day camera • Low power consumption • Very low weight (Controp, n.d.)
  • 9. Control Hardware • Ruggedized tablet • Touchscreen • Preloaded software • Internet connectivity
  • 10. Software • Easy to use • Touchscreen tablet included • Programmable autonomous flight plan • Manual operation • Autopilot • Camera operated through touchscreen
  • 11. Performance/Endurance • Capable of 2.5 hours of flight • Line of Sight connectivity • 2.5 km range
  • 12. Desired Launch and Recovery site • Clear area that is 20 ft x 20 ft • Will allow for any wind corrections and site familiarity • Platform has fixed landing skids similar to helicopter • Skids are made of 3D printed plastic • Easy to repair/replace
  • 13. Computer Aided Design (CAD) Computer simulations will help determine : • Performance needs • Energy consumption • Fuel burn • Estimated noise output • Aerodynamic properties • Capabilities/limitations
  • 14. Test and Evaluation (phase one) • Conducted in rural area to ensure safety • Validation of computer simulations • Conduct take-off, landing, and endurance • Limit altitude to max 20 ft. • Gather data for follow on testing
  • 15. Test and Evaluation (phase two) • Conduct full test of sensor package • Testing will be done at military urban training environment • Testing will help improve software
  • 16. Final Test/Customer Validation • Flight over live construction site • Flight will be no less than 2 hours • Show take-off and landing • Let stakeholders test the ease of use of the software • Show resiliency to outside frequencies from construction site • “inspect” building frame • Last stage of development prior to final agreement and product delivery
  • 17. Final Product Delivery Timeline Design phase • 3 months for product design and computer simulation Manufacturing • 1 month to order and fabricate parts • 2 weeks to test part compatibility and assemble Testing 1st phase – 1 week of flight testing • 1 week to improve autopilot and flight profiles 2nd phase – 1 week of urban environment testing • Test sensor and software usability Final phase – Live customer test • Full capability verificaiton