Drone specs.docx

ODNR Division of Wildlife Specifications for 3 Standalone UAV (Drone) Systems Each UAV system will be an identical turn-key electric quadcopter system model Matrice M30T manufactured by DJI with rechargeable batteries and charger meeting the following minimum requirements:

· Must be capable of a minimum of 14-kilometer transmission range with no loss of signal

· Fully charged batteries will provide a minimum flight time of 40 minutes

· Must include additional batteries and a charger enabling continuous operation (less battery exchanges) with a purchaser provided 2000 watt, 120V A/C power supply without damaging batteries

· Batteries must be swappable without completely shutting down the aircraft facilitating quick returns to duty after battery exchanges

· Aircraft must hold a minimum of IP55 resistance rating against dust and water

· Must include radio control transmitter with an integrated operator screen of a 7 inch minimum size and ability to connect to a larger display via wired connection and rechargeable battery and appropriate charger

· Transmitter must hold a minimum of IP54 resistance rating against dust and water

· Aircraft capable of flight operations in temperatures ranging from -20° to 50° C

· Must include software capable of live mission recording with subject tracking capability

· Aircraft, spare batteries, and radio controller must be capable of being stowed in a single durable, protective, and weather resistant case, which will fit within a typical law enforcement patrol vehicle

· Must include a self-powered and rechargeable with ability for continuous operation on purchaser provided 120V A/C or purchaser provided 12V D/C, optional use, portable 24-inch display screen for additional viewers which may be manufactured by other than DJI, in a durable, protective, and weather resistant case.

· Must include ability to determine and display to users, points on Earth in latitude/longitude coordinates

· Must include a repair kit with necessary and commonly used hand tools, commonly used fasteners, and 2 spare pairs of each type of propellor used on the aircraft

· Aircraft must have the following capabilities at a minimum:

· Angular Velocity: Pitch: 150°/sec.; Yaw: 100°/sec

· Tilt Angle: 35°

· Ascent/Descent Speed: 6 m/s, 5 m/s

· Tilt Descent Speed: 7 m/s Horizontal Speed: 23 m/s

· Service Ceiling Above Sea Level (without other payload not in this list of specifications): 5,000 m

· Wind Resistance: 12 m/s

· Real-time Kinematic Positioning Accuracy (fixed RTK enabled):

1 cm+1 ppm (horizontal) 1.5 cm+1 ppm (vertical)

· Hovering Accuracy (windless or breezy):

Vertical: ±0.1 m Horizontal: ±0.3 m

· Aircraft must include a camera gimbal with the following minimum capabilities:

· Angular Vibration Range: ±0.01°

· Controllable Range: Pan: ±90°, Tilt: -120° to +45°

· Mechanical Range: Pan: ±105°, tilt: -135° to +60°, Roll: ±45°

· Aircraft must include a zoom camera with the following minimum specifications:

· Sensor: 1/2" CMOS, Effective pixels: 48M

· Lens: Focal length: 21-75 mm (equivalent: 113-405 mm) Aperture: f/2.8-f/4.2

· Focus: 5 m to ∞

· Exposure Compensation: ±3 ev (using 1/3 ev as step length)

· Electronic Shutter Speed: Auto Mode: Photo: 1/8000-1/2 s Video: 1/8000-1/30 s Manual Mode: Photo: 1/8000-8 s Video: 1/8000 -1/30 s

· ISO Range: 100-25600

· Video Resolution: 3840×2160

· Photo Size: 8000×6000

· Aircraft must include a wide-angle camera with the following minimum specifications:

· Sensor: 1/2" CMOS, Effective pixels: 12M

· Lens: DFOV: 84°

· Focal length: 4.5 mm (equivalent: 24 mm) Aperture: f/2.8

· Focus: 1 m to ∞

· Exposure Compensation: ±3 ev (using 1/3 ev as step length)

· Electronic Shutter Speed: Auto Mode: Photo: 1/8000-1/2 s Video: 1/8000-1/30 s Manual Mode: Photo: 1/8000-8 s Video: 1/8000-1/30 s ISO Range: 100-25600

· Video Resolution: 3840×2160 Photo Size: 4000×3000

· Aircraft must include a thermal imaging camera with the following minimum specifications:

· Thermal Imager: Uncooled VOx Microbolometer Lens: DFOV: 61°

· Focal length: 9.1 mm (equivalent: 40 mm) Aperture: f/1.0

· Focus: 5 m to ∞

· Sensitivity: ≤30 mk@F1.1

· Infrared Temperature Measurement Accuracy: ±2°C or ±2% (using the larger value)

· Video Resolution: Infrared Image Super-resolution Mode: 1280×1024 Normal Mode: 640×512

· Photo Size: Infrared Image Super-resolution Mode: 1280×1024 Normal Mode: 640×512

· Pixel Pitch: 12 um

· Temperature Measurement Method: Spot Meter, Area Measurement

· Temperature Measurement Range: High Gain Mode: -20° to 150° C (-4° to 302° F) Low Gain Mode: 0° to 500° C (32° to 932° F)

· Temperature Alert Supported

· Palette: White Hot/Black Hot/Tint/Iron Red/Hot Iron/Arctic/Medical/Fulgurite/Rainbow 1/Rainbow 2

· Aircraft must include a First Person View Camera with the following minimum specifications:

· Resolution: 1920×1080

· DFOV: 161°

· Frame Rate: 30 fps

· Aircraft must include laser range finding capability with the following minimum specifications:

· Measurement Accuracy: ± (0.2 m + D×0.15%) D is the distance to a vertical surface

· Measuring Range: 3-1,200 m (0.5×12 m vertical surface with 20% reflectivity)

· Aircraft must include a vision system with the following minimum specifications:

· Obstacle Sensing Range: Forward: 0.6-38 m, Upward/Downward/Backward/Sideward: 0.5-33 m FOV: 65° (H), 50° (V)

· Operating Environment: Surfaces with clear patterns and adequate lighting (> 15 lux)

· Aircraft must include a searching spotlight and a public address loudspeaker

· Aircraft must include navigation lighting per FAA regulations

· Vendor to provide delivery and 2 hours of operation training per system specific to the model at a location within the State of Ohio.

· Vendor to provide preventative maintenance for a period of 2 years post-delivery and unlimited function checks upon request for the life of each system.