### Exhibit F Pinnacl X Description of Aircraft System s

Chameleon Pro Description of Aircraft System:

Chameleon Pro manufactured by Pinnacl X

Visual Observer and Pilot Controllers

Website: www. pinnaclx.com

Chameleon Pro Product description:

The Chameleon Pro quadrotor, is a small unmanned aerial system (sUAS) that's been de signed to carry

wireless video and still cameras that weighs less than 453 grams . Radio control is used to pilot the sUAS

remotely, semi autonomously and autonomously. A ground control stat ion is used to assists the pilot.

The major flight modes are: manu al, altitude hold, loiter mode and autonomous

. The manual flight

mode requires the pilot to fly the Chameleon Pro at all times. If the pilot lets go of the control sticks the

### Exhibit F Pinnacl X Description of Aircraft System s

aircraft will r esume a level attitude only. It will drift and change altitude. The altitude hold mode the

aircraft will maintain its current altitude and if the pilot lets go of the control sticks the aircraft will

maintain a level attitude and current altitude with the throttle control at the middle position. The

aircraft will drift. The loiter mode allows the pilot to let go of the controller and the aircraft will stop and

maintain its position, dependent on GPS signal strength. The autonomous mode will command the

air craft to fly a preprogrammed path uploaded from the ground control station, required GPS signal and

ground control station for more than one flight routine. The return to land mode will command the

aircraft to fly back to the starting point at a preprogram med altitude, GPS signal required. The pilot can

always override all flight modes by operating the controller direct ly , or by flipping a switch changing the

flight modes. A GEO fence can be activated from the ground control station which will not allow the

aircraft to fly beyond a boundary and altitude specified by the operator. The usage of the GEO fence

requires a good GPS signal. The GEO fence will fail in the event of a GPS signal loss and the aircraft will

not be limited to remain in a defined area. To prevent a flyaway situation with a poor GPS signal an

additional feature is programed into the auto pilot which is the GPS fail safe mode. In the event of a GPS

signal reduction to a poor GPS signal the auto pilot will switch modes to altitude hold mode a nd the pilot

will be required to fly the aircraft manually. Arm bolts, motor bolts and ESC wiring are exposed for

preflight inspection.

Chameleon Pro Features

 Plastic or Carbon fiber rotors

 Brushless electric motors

 1 Barometric pressure sensor: Meas ures altitude.

 1 GPS Receiver: Measures absolute position with a resolution of 2.0 meters when the GPS signal

strength is at maximum

 Auto stabilization and onboard sensors and processor

 3 Gyros: Monitors the rate of rotation about the X, Y and Z axis

 3 Ac celerometers: Monitor the rate of acceleration in the X, Y and Z directions

 3 Axis Magnetometer: Allows the quadrotor to orient itself relative to the Earth’s magnetic field

Technical Specifications:

Dimensions:

 Width: 14.25 inches (362 mm)

 Length 12.5 inches ( 372 mm)

 Height: 3.75 inches (95.3 mm) (with 1.3 inch landing gear)

Weight and Payload

 Quadrotor Weight (with battery 5100 mah 3S): 2.8 Lb ( 1,282 grams)

 Payload Capability: 1 Lb (453 grams)

 M aximum Gross Take

- Off Wight: 3.8 Lb ( 1,735 grams)

Flight Characteristics

 Maximum Climb Rate: 7.6 m/s (1,500 ft/min)

o Autopilot must be in stabilize mode

 Descent Rate: 7.6 m/s (1,500 ft/m)

### Exhibit F Pinnacl X Description of Aircraft System s

o Autopilot must be in stabilized mode

 Turn Rate: 100 Degrees/second

 Maximum Speed: 32 km/hr (20 mph)

o Autopilot must be in stabilized or attitude mode

 Minimum Speed: 0 Km/hr (0 mph)

 Launch Type: VTOL (Vertical Takeoff and Landing)

 Maximum Flight Time: 16 to 22 minutes ( depending on payload )

Rotor Blades (Propellers)

 Four Opposing Rotation (Four Propellers Total)

 Rotor Blade Material: Plastic Molded Carbon Fiber

 Rotor Diameter: 9.5 or 10 inches (241.3 mm or 254mm )

 Rotor Weight: .0 25 Lb (1 1 grams or 13 grams )

Landing Gear

 Installed Height: 1.3 or 6 inches (33 mm or 152.4mm )

 Stance Width: 14.25 inches (362 mm)

 St ance Length: 12.5 inches (318 mm)

 Landing Gear Material: ABS Plastic

Frame Materials

 Carbon Fiber/Fiber Glass

 Plastic

 Aluminum, Nylon and Stainless Steel Fasteners

Electric Motors

 Brushless Motors: 4

 Configuration: Direct Drive (One Motor per Rotor)

 Ball Bearing on each motor

 Rotor Mounting Points: 4 bolt

Rechargeable Quadrotor Battery

 Cell Chemistry: Lithium Polymer

 Voltage: 11.1, V nominal

 Capacity: 3S, 5100 mah

 Connectors: Integrated Balance and Power

 Recharge Time: 1.2 hours (After typical flight)

### Exhibit F Pinnacl X Description of Aircraft System s

Optional Camera Attachments

 GOPRO camera or equivalent

o GOPRO Mounts fixed, two axis tilt and yaw, gimbal with tilt

 Canon A2200 or equivalent

o Canon mount single axis tilt, two axis tilt and yaw

 FLIR thermal imaging or equivalent

o FLIR mount single axis tilt, two axis tilt and yaw

Position Lights and Status Lights

 LED light s, white and red

 Autopilot status light

Operating Requirements

 Recommended Pre

- Use Temperature 10 to 35 degrees C ( 50 to 95 degrees F)

 Maximum Environmental Operating Temperature:

- 7 to 38 degrees C (20 to 100 degrees F)

 Relative Humidity: 0% to 90% Noncondensing

 Maximum Wind Speed: Varies based on payload an miss ion (32 km/h [20 mph])

Control Station

One control station with a 2.4GHz, Spread Spectrum link for pilot

One control station with a 2.4GHz, Spread Spectrum link for observer

 Transmission Technique: FHSS Frequency Hopping Spread Spectrum

 Frequency band: 2.400

- 2.4835 Ghz

 Certifications: CE, FCC, IC, ETSI

 Receiver Channel Selection: Automatic (13 Channels) Quadrotor Antenna: Wired Whip Antenna

Communication System Description

RF Communications

9 15 Mhz Data Link

 Link Type: Quadrotor to ground and ground to quadrotor (Two

- Way)

 Quadrotor Antenna: Wired Whip Antenna in cased in a plastic housing

 Transmission Power: 100 mW

 Receiver sensitivity:

- 100dBm

Video Transmission

5.8GHz Video Link

 Link Type: Quadrotor to ground (One

- Way)

 Quadrotor Antenna: Wired Whip Antenna

 Transmission power: 25 0 mW

 Receiver sensitivity:

- 90dBm

 Transmission Technique: Single Channel

 Frequency band: 5705

- 5945 Ghz

### Exhibit F Pinnacl X Description of Aircraft System s

 Certifications: CE, FCC, IC, ETSI

 Data Link Channel Selection: Manual (8 Channels)

Chameleon Pro Handheld Controller, Observer and Pilot

 Width 7 inch (177.8mm)

 Height: 7 inch (177.8mm)

 Depth: 3.1 inches (79mm)

 Weight: 1.54Lb (700 grams)

11 Onboard Sensors

 3 Solid State MEMS (Micro

- Electro

- Mec hanical Systems) Gyros

 3 Solid State MEMS (Micro

- Electro

- Mechanical Systems) Accelerometers

 3 Magnetometers (Magnetoresistive Sensors)

 1 Barometric Pressure Sensor

 1 GPS Receiver

GPS

 GPS Used For: Position Hold, Location and Velocity Data

 Maximum Satellites Tracked Simultaneously: 16

 Position Update Rate: 4 Hz

 GPS Antenna: Ceramic Patch

Flight Data Recorder

 Flight Data Recording: On

- Board

 Flight Data Recording: On the ground control station

 Fl ight Data Storage: Removable 2GB MicroSD M emory Card

 Data Recorded: Onboard Sensor Flight Data (Link quality, Orientation, Altitude, Speed and

Direction)

### Exhibit F Pinnacl X Description of Aircraft System s

DJI S1000 , Octorotor Description of Aircraft Systems

DJI S1000 Octorotor, manufactured by DJI

See Exhibit K S1000 User’s Manual

DJI S900, Hexrotor Description of Aircraft Systems

See Exhibit M S900 User’s Manual