### Exhibi t F

- 2 Pinnacl X Description of Fixe d Wing Aircraft System s

Needs a manual and operating procedures and training

Ultra Stick sUAS Description of Aircraft System:

Ultra Stick s UAS , 25e and 120 Aircraft Manufactured by Pinnacl X

(The 120 is the larger aircraft)

Visual Observer and Pilot Controllers

Website: www. pinnaclx.com

Ultra Stick sUAS Product description:

The Ultra Stick sUAS fixed wing aircraft , is a small unmanned aerial system (sUAS) that's been de signed

to carry payloads that include wireless video and still cameras that weighs less than 12.57 kg (27.7 Lb)

. Radio control is used to pilot the sUAS remotely, semi autonomously and autonomously. A ground

control station is used to assists the pilot. The major flight modes are: manu al, semi

- autonomous , loiter

,

autonomous and return to land

. The manual flight mode requires the pilot to fly the aircraft at all times.

### Exhibi t F

- 2 Pinnacl X Description of Fixe d Wing Aircraft System s

The semi

- autonomous mode

, the aircraft will maintain a level attitude and current altitude if the pilot

lets go of the control sticks with the throttle co ntrol at the middle position

. The loiter mode allows the

pilot to let go of the controller and the aircraft will fly around a GPS waypoint . The autonomous mode

will command the aircraft to fly a preprogrammed path uploaded from the ground control station,

required GPS signal and grou nd 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 preprogrammed altitud e . 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 th e GPS fail safe mode. In the event of a GPS

signal reduction to a poor GPS signal the auto pilot will switch modes to semi

- autonomous hold mode

and the pilot will be required to fly the aircraft manually. Typically

, fixed wing aircraft always receive a

go od GPS signal since they must be flown in an open area.

Ultra Stick sUAS Features

 Plastic or Carbon fiber propeller

 Brushless electric motor

 1 Barometric pressure sensor: Measures altitude.

 1 GPS Receiver: Measures absolute position with a resolution o f 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 Accelerometers: Monitor the rate of acceleration in the X, Y and Z directions

 3 Axis Magnetometer: Allows the fixed wing aircraft to orient itself relative to the Earth’s

magnetic field

Technical Specifications Ultra Stick sUAS 120 :

Dimensions:

 Width: 75.6 inches ( 1920 mm)

 Length 68.1 inches ( 1730 mm )

 Height: 12 inches ( 305 mm) ( with landing gear)

Weight and Payload

 Aircraft Weight (with battery 5100 mah 3S): 15.6 Lb ( 7070 grams)

 Payload Capability: 12.1 Lb (5500 grams)

 M aximum Gross Take

- Off Wight: 27.7 Lb ( 12570 grams)

Flight Characteristics

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

o Must be in manual mode

 Descent Rate: 7.6 m/s (1,500 ft/m)

o Must be in manual mode

### Exhibi t F

- 2 Pinnacl X Description of Fixe d Wing Aircraft System s

 Maximum Speed: 92 mph ( 41 m/s )

o Any mo de

 Minimum Speed: 13 mph ( 6 m/s )

 Launch Type: Runway launch

 Maximum Flight Time: 20 to 6 0 minutes ( depending on payload )

Propeller

 Propeller Material: Plastic Molded Carbon Fiber

 Propeller : 14 x 9.5 fixed or folding

 Propeller Weight: Fixed, .066 Lb ( 30 grams )

Technical Specifications Ultra Stick sUAS 25e :

Dimensions:

 Width: 75.6 inches (1270 mm)

 Length 68.1 inches (1090 mm)

 Height: 8 inches (203.2mm) (with landing gear)

Weight and Payload

 Aircraft Weight (with battery 5100mah 3S): 4.53 Lb (1960 grams)

 Payload Capability: 5 Lb (2250 grams)

 Maximum Gross Take

- Off Wight: 9.3 Lb (6460 grams)

Flig ht Characteristics

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

o Must be in manual mode

 Descent Rate: 7.6 m/s (1,500 ft/m)

o Must be in manual mode

 Maximum Speed: 58 mph (26 m/s)

o Any mode

 Minimum Speed: 11 mph (5 m/s)

 Launch Type: Runway launch

 Maximum Flight Time: 20 to 40 minutes (depending on payload)

Propeller

 Propeller Material: Plastic Molded Carbon Fiber

 Propeller: 12 x 6 fixed or folding

 Propeller Weight: Fixed, .04 Lb (18 grams)

Technical Specifications for Ultra Stick sUAS 25e and 120 :

Landing Gear

 Aluminum frame, inflated rubber tires

Frame Materials

 Built up balsawood and plywood with Carbon Fiber/Fiber Glass Spar

### Exhibi t F

- 2 Pinnacl X Description of Fixe d Wing Aircraft System s

 Built up balsawood and plywood Wing with plastic file coating

Electric Motor

 Brushless Motors

 Configuration: D irect Drive (One Motor )

 Ball Bearing on each motor

 Motor Mounting Points: 4 bolt

Rechargeable Aircraft Battery

 Cell Chemistry: Lithium Polymer

 Voltage: 11.1, V nominal

 Capacity: 3S, 5100 mah

 Connectors: Integrated Balance and Power

 Rec harge Time: 1.2 hours (After typical flight)

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 i maging or equivalent

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

Position Lights and Status Lights (optional)

 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])

 Store in a cool location away from the sunlight

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 Fr equency 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

### Exhibi t F

- 2 Pinnacl X Description of Fixe d Wing Aircraft System s

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

 Certifications: CE, FCC, IC, ETSI

 Data Link Cha nnel Selection: Manual (8 Channels)

Ultra Stick sUAS Handheld Controller, Visual 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

- Elec tro

- Mechanical 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 Memory Card



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

Direction