## DESCRIPTIVE DATA

Components

Note: Components subject to change.

Airframe

Configuration: Quad Copter

Manufacturer: PMG Multi

- Rotors

Model: RECON Professional Grade Quad Copter

Size: 1045mm Diagonal

Material: FR4, Polycarbonate

Number of Boom Arms: 4

Motors

Number of Motors: 4

Type : 3 Phase Brushless Electric

Manufacturer: PMG

Model: 4114

Per Motor Max Power: 299 W

Per Motor Max Current: 36 A

Motor Operating Voltage: 6S

Weight : 1 45 g

Electronic Speed Controllers

Number of ESC: 4

Type: Opto Non BEC

Manufacturer: PMG

Model: 40A OPTO ESC

Refresh Rate: 30 Hz

- 450Hz

Drive PWM Frequency : 8KHz

Weigh (with radiators) : 20 g

Max Current: 40A

ESC Operating Voltage: 6 S (29.6V nominal)

Propellers

Number of Props: 4

Type: Fixed Pitch

Manufacturer: PMG

Model: 15 x 5 .5 /15 x 5 .5 R

Flight Controller

Manufacturer: DJI

Model: A2

C2 Radio Control Tx / Rx

Type: 2.4GHz FAS STest

Manufacturer: Futaba

Model: 14SG

Number of Channels: 14

Transmitter:

Receiver: Futaba R 7008SBMain Bus Batteries

Number of Batteries: 2

Type: Lithium Polymer (LiPo)

Manufacturer: Various

Voltage: 6S

Current: 5 000mAh ea.

Weight: 770 g (average)

Discharge Rating: 30C

Max Continuous Discharge: 30C

Power Distribution

Main Bus Power Distribution

- Manufacturer / Model: PMG (Top Frame PCB)

Current Capacity: 20 0A

Number of Outputs: 8

Voltage Output: 12V

– 25V

OSD / Telemetry Downlink

Manufacturer: DJII OSD Mark II

Data Transmission / Frequency: PAL/NTSC

Aircraft Telemetry Data:

Voltage

Channel

Distance Aircraft to Home

Altitude

Control Mode

F ail

- safe Mode

Pitch Attitude

Roll Attitude

Attitude Line

Flight Velocity

GPS Satellite

Video Input

Ground Station

Manufacturer: DJI

Properties

Altitude

Latitude

Longitude

Forward Flight Speed

Turn Mode

Head Degree

Hold TimeAssignments

Camera Shutter

Gimbal Control

Airdrop Control

General Purpose Control

Mission Mode

Continuous / Start to End

Turning Mode

Stop and Turn / Bank Turn / Adaptive Bank Turn

Map Browser

Google Earth 3

- D GIS

Safety Control

Automatic Hovering & Go Home Function

Strictly AI Control Logic Design

Flight Instruments

GPS Coordinates Indicator

General Speed Indicator

Attitude Indicator

RF Signal Strength Indicator

Helicopter Position Tracker

Pitch Position %

Throttle Position %

Servo Voltage

Communication

Hardware Interface: RS

- 23 2

Radio Frequency: 900 MHz/2.4 GHz

Data

- Throughput: Maximum 11,5200 bps

Rotorcraft Control Modes

Manual Mode

Attitude Mode

GPS Attitude Mode

GPS Cruise Mode

Way Point Mode

Joystick Mode

Keyboard Mode

Pre

- Flight Simulation

Virtual environment aid to help users get familiar with operations

## SPECIFICATIONS

Diagonal Wheelbase : 860 mm

Frame Arm Length : 310 mm

Frame Arm Weig ht (with Motor, ESC, Propeller) : 32 3 g

Center Frame Width : 245 mm

Center Frame Length : 420 mm

Center Frame Weight (with Landing Gear Mounting Base, Servos) : 637 g

Landing Gear Size : NA

Current Spec Gross Weight: 3.8 Kg

Current Spec Empty Weight (excluding batteries): 1.9 Kg

Current Spec Payload (including batteries): 1.9 Kg

Max Gross Weight: 6 Kg

Performance

Flight Duration: 30 min @ current spec, 2 0 % battery capacity remaining

Range: 3 000 ft. demonstrated RF link (note: UAS will be limited to LOS operations)

Speed Range: 0

– 40 kt demonstrated

Max Altitude: 2000ft+ estimated (note: UAS will be limited to 400ft AGL or below)

Wind Operation: 15kt+ demonstrated



## LIMITATIONS

Aircraft

Max Takeoff Weight: 6 kg

Max Forward Airspeed Limit: 50kt (FAA regulatory)

Max Altitude: 400ft AGL or 200ft above an elevated platform (FAA regulatory)

Max Range: LOS (FAA regulatory)

Max Flight Duration: 30 minutes (FAA regulatory)

Mains System Voltage Parameters: 29.6V minimum / 33.6V maximum

Minimum Allowable Remaining Battery Capacity: 25% (FAA regulatory)

Max Motor Temperature: 62oC

Max ESC Temperature: 51oC

COG Balance Limits: Within 3% of CG on X / Y axis

Max Angle of Bank: 4 5o