UAV prototype for terrain dose-rate mapping Eng. Diego Garca - - PowerPoint PPT Presentation

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UAV prototype for terrain dose-rate mapping Eng. Diego Garca - - PowerPoint PPT Presentation

UAV prototype for terrain dose-rate mapping Eng. Diego Garca (CNEA-UTN) diegogarcia@cae.cnea.gov.ar Eng. Lucio Martinez Garbino (CNEA-UTN) luciojmg@cae.cnea.gov.ar 1 Origins of the project AGE CNEA-CAE requires a surface dose rate map


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UAV prototype for terrain dose-rate mapping

  • Eng. Diego García (CNEA-UTN) diegogarcia@cae.cnea.gov.ar
  • Eng. Lucio Martinez Garbino (CNEA-UTN) luciojmg@cae.cnea.gov.ar
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Origins of the project

 AGE CNEA-CAE requires a surface dose rate map  Large measuring area (8km2), requires automated process  Requires periodic measurements  Due to possible high dose levels prefer to reduce the exposure of people  GIAR works on a project for multipurpose flying vector

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Particular conditions

 Rough terrain  Inaccessible areas and obstacles (perimeter fencings)  Requires static measurements (depends on detector volume vs exposition time)

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Objectives of the project

  • Mechanicals

 Light  Robust

  • Measurement

 Count measurement with geospatial reference  Detection efficiency  Telemetry

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Requirements of project

  • Navigation

 Autonomy  Controllability (altitude, full featured AP, secure mode, inertial NAV)  Telecommand (power off of not used modules)

  • Auxiliar systems

 Real time Video Link

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Our proposal

 We requires a flying vehicle (UAV). But what kind?

Feature Plane Helicopter Drone Balloon Weather sensitivity Medium Medium Medium High Autonomy Medium Low Low High Sturdiness Medium Low Medium High Maneuverability Medium High High Med-High Speed Med-High Low Med Low-static Landing requirements Medium Low Low Low Design complexity Medium High Medium Low

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Main Features

 Sonar obstacle avoidance system  Sonar altimeter  AHRS system (IMU)  Video link  Autopilot  Real time telemetry and telecommand  Entirely designed and build by us. All materials available off-the-shelf  Up to 6 hours autonomy  Easy scalability (more Helium, more payload)  Very low cost (USD 600), without detector

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Legal, regulatory and safety

 ANAC (National Civil Aviation Association) (UAV, Res. Nº527/2015)  Helium (instead of heated air or Hidrogen)  Negative floatability  Secure mode Auto Pilot (3 modes)  Shut-off  Return to base  Secure landing

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Other features

 3D surface map  Gamma Ray Spectrometry  Microcontroller based for low count rate  FPGA based for high count rates

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Future Works

 Plastic detectors  Silicon PMT  High precision GNSS (Global Navigation Satellite System)  Relation between measure time and weight of scintillator material and volume  Background characterization

Calibration

 Measure counts by a Scintillator (NaI(Tl))

  • need to convert to dose rate
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Interface Prototype

Video with Head up display Navigation Log Emergency settings Count, spectrum and alarm Warnings and alarms panel Nav sonar AP panel Map and WP display ECAM panel (Electronic Centralised Aircraft Monitor) Power control, battery state, ammeter, autonomy

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Vehicle Prototype

2 vectored motors NAV sonar Video cammera Lipo battery pack and balancer Carbon fiber structure Electronics Detector NAV, Strobe, ATTR lights

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UAV prototype for terrain dose-rate mapping

  • Eng. Diego García (CNEA-UTN) diegogarcia@cae.cnea.gov.ar
  • Eng. Lucio Martinez Garbino (CNEA-UTN) luciojmg@cae.cnea.gov.ar