Page 1 ® INTEL FALCON™ 8+ Unmanned Aircraft System REV 00 APR 2017...
Page 4 To the extent permitted by applicable law, Intel disclaims all liability for any damages, direct or indirect, arising from the use of the unmanned aircraft system (UAS) outside of its intended use, in breach of Intel Corporation’s Safety Guidelines, Safety Precautions or any other...
Page 5 No license of any kind, whether express, implied, statutory, by estoppel or otherwise to any intellectual property rights, technology, software, in each case whether in whole or part, is granted by Intel, or any of its subsidiaries, in this User Manual. For permission requests, write to the licensee, addressed Attention: Permissions Coordinator (RE: ISBN 978-1-945746-94-9) at the address below.
Page 7: Record Of Revision
RECORD OF REVISION REVISION NUMBER REVISION DATE REVISION NUMBER REVISION DATE Original Issue APR 2017 RECORD OF REVISION © 2017 Intel Corporation. All rights reserved. REV 00 APR 2017...
Page 9: Table Of Contents
WEIGHT LIMITS ............................18 CENTER OF GRAVITY LIMITS ....................... 18 FLIGHT AND MANEUVER LIMITATIONS ..................18 2.7.1 Minimum Crew Requirement ......................19 ENERGY LIMITATIONS ..........................20 TABLE OF CONTENTS © 2017 Intel Corporation. All rights reserved. REV 00 APR 2017...
Page 10 SITE SETUP PROCEDURE ........................34 ASSEMBLING THE UAS ........................... 36 4.3.1 Installing the Camera Mount ......................36 4.3.2 Payload and Compass Calibration ....................37 CHECKLIST PROCEDURES ........................39 TABLE OF CONTENTS © 2017 Intel Corporation. All rights reserved. REV 00 APR 2017...
Page 11 SECTION 7 AIRCRAFT AND SYSTEMS DESCRIPTION ......................64 AIRFRAME ..............................64 7.1.1 Central Unit ............................. 65 7.1.2 Carbon Cross ............................66 7.1.3 MOTOR RAILS AND PROPELLERS ....................66 7.1.4 ELECTRICAL SYSTEM ......................... 67 TABLE OF CONTENTS © 2017 Intel Corporation. All rights reserved. REV 00 APR 2017...
Page 12 MAINTENANCE MANUAL ® INTEL FALCON™ 8+ UAS 7.1.5 LIGHTING SYSTEMS - EXTERIOR LIGHTING ................73 INTEL® COCKPIT GROUND CONTROL STATION ................. 74 7.2.1 Intel ® Cockpit GCS Control Unit ...................... 75 7.2.2 Overview of the Status Display Controls ..................77 7.2.3 Normal Operation: Preparing the Intel...
Page 13 INTRODUCTION ............................136 10.1.1 Intended Use ............................136 10.1.2 Safety Guidelines ..........................136 10.1.3 Weather ..............................139 10.1.4 Terrain ..............................139 10.1.5 Accident/Incident Reporting ......................140 TABLE OF CONTENTS © 2017 Intel Corporation. All rights reserved. REV 00 APR 2017...
Page 15: Section 1 General
Falcon™ 8+ Unmanned Aircraft System (UAS) is the first-choice multi-rotor for the most challenging professional UAS inspections and surveying operations. Small and portable with a maximum take-off weight of only 2.8 kg, but with a payload weight of 0.8 kg, the Intel ®...
Page 16: Copyright Notice
The authors and publishers have attempted to trace the copyright holders of all materials produced and apologize to copyright holders if permission to publish in this form has not been obtained. If any copyright material has not been acknowledged, please write to Intel Corporation.
Page 17: Model Applicability
Intel Corporation will correct any errors, inaccuracies or omissions as soon as practicable. Intel Corporation disclaims all liability for any damage arising from the use of this documentation.
Page 18: Three View - Normal Ground Altitude Figure
2200 MISSION COLLEGE BLVD SANTA CLARA, CA 95054 Intel Corporation reserves the right to change, amend or update all available documents at any time and without notice. Contact an Intel Corporation representative to obtain the latest unmanned aircraft specifications and roadmaps.
Page 19: Descriptive Data
16 – 26 min; varies based on payload weight, battery conditions, and MAX FLIGHT TIME environmental conditions 1.3.2 Battery System SYSTEM POWER ENDURANCE Aircraft Intel Powerpack 4000 mAh 26 min GENERAL © 2017 Intel Corporation. All rights reserved. REV 00 APR 2017...
Page 20: Propulsion System
Operating Frequencies COMMAND AND CONTROL 2.4 GHz Spread Spectrum VIDEO 5.8 GHz frequency band Command Link Range COMMAND AND CONTROL 4921 feet (1500m) VIDEO 0.34 mi (550 m) GENERAL © 2017 Intel Corporation. All rights reserved. REV 00 APR 2017...
Page 21: Symbols, Abbreviations And Terminology
Meter Meters per Second Miles Miles per Hour Millimeter Milliampere Hour Milliwatt Minute NOTAM Notices to Airmen RPIC Remote Pilot-in-Command Pounds Unmanned Aircraft System Volt Visual Observer Watt GENERAL © 2017 Intel Corporation. All rights reserved. REV 00 APR 2017...
Page 23: Section 2 Limitations
SECTION 2 LIMITATIONS INTRODUCTION The limitations section contains only those limitations required by regulation or that are necessary for the safe operation of the Intel ® Falcon™ 8+ Unmanned Aircraft System (UAS), including the power plant, systems, and equipment. It includes operating limitations, instrument markings, and basic placards.
Page 24: Weight Limits
® without a payload or with an approved camera and gimbal mount. CAUTION: WHEN INSTALLING A NEW PAYLOAD ONTO THE INTEL® FALCON™ 8+ UAS, IT IS NECESSARY TO PERFORM A PAYLOAD CALIBRATION AND A COMPASS CALIBRATION. CALIBRATIONS WILL BE SAVED AND RECALLED OIN FUTURE FLIGHTS.
Page 25: Minimum Crew Requirement
Intensive training of every Remote Pilot to operate the UAS in all flight modes is mandatory. Training is provided by authorized training providers; contact an Intel Corporation representative. The Visual Observer (VO) is responsible for monitoring area of operations for airborne, environmental hazards, and for ground-based hazards.
Page 26: Energy Limitations
OTHER LIMITATIONS Do not make any unapproved modifications to the Intel ® Falcon™ 8+ UAS. Do not transport the system in containers not approved by Intel Corporation. Do not disassemble the aircraft. 2.9.1 GPS Mode In this mode the inputs via the Intel ®...
Page 27 The GPS receiver module of the Intel ® Falcon™ 8+ UAS is placed directly underneath the canopy of the central unit and is surrounded by an antenna. The canopy of the Intel ® Falcon™ 8+ UAS is made from a material which does not influence the satellite signals, but anything on the top of the Intel ®...
Page 28: Height Mode
Ascend rate is limited to 3 m/s.  Descend rate is limited to 3 m/s. WARNING: AVOID FULL CONTROL STICK INPUTS IN HEIGHT-MODE! THE INTEL® FALCON™ 8+ UAS CAN BE OVERSTRESSED IN CERTAIN SITUATIONS SUCH AS FLYING ABRUPT MANEUVERS WITH A LOW BATTERY.
Page 29 Use the right control stick to keep the current position as precisely as possible, while carefully moving down the left control stick to descend slowly.  Move the left control stick fully down to land the UAS. While the Intel ® Falcon™ 8+ UAS is on the ground with running Motors, always keep the left control stick in the fully downward position to avoid any unintentional take-off.
Page 30: Placards
Falcon™ 8+ UAS Serial Numbers can be found on the rear side of the Central Unit. 2.10.2 Remote Controller The remote controller is placarded with regulatory approval labels that match the transceivers within. LIMITATIONS © 2017 Intel Corporation. All rights reserved. REV 00 APR 2017...
Page 32: Section 3 Emergency Procedures
3. Flight Path Monitor 4. Shutdown Checklists Complete FIRES 3.6.1 During Start on Ground 1. Left Control Down 2. START/STOP Switch 1 second 3. Shutdown Checklists Complete EMERGENCY PROCEDURES © 2017 Intel Corporation. All rights reserved. REV 00 APR 2017...
Page 33: Electrical Fire In Flight
LEAD TO UNEXPECTED POSITIONAL CHANGES OF THE SYSTEM. WARNING: THE SYSTEM MUST BE LANDED BY THE REMOTE PILOT AS THERE IS NO AUTO- LANDING IN CASE OF LOW BATTERY. EMERGENCY PROCEDURES © 2017 Intel Corporation. All rights reserved. REV 00 APR 2017...
Page 34: Loss Of Electrical Power
When there is only one minute Vibration of the Intel ® remaining flight time left, the Cockpit GCS every 10 Intel ® Cockpit GCS will vibrate seconds every 10 seconds. EMERGENCY PROCEDURES © 2017 Intel Corporation. All rights reserved. REV 00 APR 2017...
Page 35: Lost Link
295 fpm (1.5 m/s) until it lands. CAUTION: IF THE INTEL® POWERPACK™ BATTERIES ARE LOW AT THE END OF A FLIGHT, THE EXTRA POWER NEEDED TO ASCEND COULD DEPLETE THE INTEL® POWERPACK™...
Page 36: Loss Of Navigation System
® INTEL FALCON™ 8+ UAS CAUTION: IN A SITUATION WITHOUT GPS SIGNAL, THE INTEL® FALCON™ 8+ UAS WILL DRIFT WITH THE WIND WHILE DESCENDING It is possible to define a new home position while the UAS is in the air.
Page 37: Loss Of Ground Control Station
In the event the Ground Control Station fails to respond to inputs: 1. Visual Contact with Aircraft Maintain Through Landing 2. Visually confirm Come Home Procedure Confirm 3. Flight Path Monitor 4. Shutdown Checklists Complete EMERGENCY PROCEDURES © 2017 Intel Corporation. All rights reserved. REV 00 APR 2017...
Page 40: Section 4 Normal Procedures
Precipitation forecast Flight Missions should be canceled/rescheduled if meteorological conditions include or forecast the following: Thunderstorms and microbursts  Tornadoes  Icing  Hail   Lightning  NORMAL PROCEDURES © 2017 Intel Corporation. All rights reserved. REV 00 APR 2017...
Page 41 Public Access Areas o Special Permission Requirements  Availability of Alternate Operating Sites  Landing Field o Area o Terrain o Obstacles surrounding field o Alternate  Contact Information NORMAL PROCEDURES © 2017 Intel Corporation. All rights reserved. REV 00 APR 2017...
Page 42: Assembling The Uas
1. Feed the Camera Mount’s carbon rod, without thumbscrew, into the hole on the front side of the Central Unit. Note: Make sure the Camera Mount comes out straight and not at an angle. 2. Adjust the Payload Adapter into place. NORMAL PROCEDURES © 2017 Intel Corporation. All rights reserved. REV 00 APR 2017...
Page 43: Payload And Compass Calibration
The first time a payload is connected with the Intel ® Falcon™ 8+ UAS, it is necessary to perform a payload calibration and then the compass calibration (strictly in that order). The Intel ® Falcon™ 8+ UAS will save the calibrations with that exact payload and remember it the next time it is used.
Page 44 FALCON™ 8+ UAS ON AN ELEVATED PLATFORM TO MAKE SURE THE PAYLOAD DOES NOT HIT THE GROUND AND CAUSE DAMAGE WHEN IT TILTS DOWNWARDS. 6. When the payload does not move anymore, switch off the payload, the Intel ® Falcon™ 8+ UAS and Intel ®...
Page 46: Preflight Inspection
Propeller which is not attached tightly enough. In this case sound can be heard. carefully check the self-tightening nut on top of the Propeller. Check the SD card in the back of the Intel ® Falcon™ 8+ UAS. If the...
Page 47: Initial Preflight
Propulsion Intel ® Powerpack™ Battery Charged, Connected Prior to each mission, charge each Intel ® Powerpack™ Battery to 100%. Replace battery if remaining charge is inadequate for planned flight time. Secure battery in aircraft in proper location with Intel label facing upward.
Page 48: Preflight
® Powerpack™ Battery for the Intel ® Cockpit GCS fully inserted, with the colored label facing downwards. 5. Intel ® Cockpit GCS condition Check no loose parts NORMAL PROCEDURES © 2017 Intel Corporation. All rights reserved. REV 00 APR 2017...
Page 49: System Start
To avoid interferences with the UAS, set all smartphones to airplane (flight) mode. SYSTEM START 1. System CAUTION: ALWAYS SWITCH ON THE SYSTEM IN THE FOLLOWING ORDER: 1) PAYLOAD 2) INTEL® FALCON™ 8+ UAS CENTRAL UNIT 3) INTEL® COCKPIT GCS 2. System Boot Triple Beep NORMAL PROCEDURES ©...
Page 50 MAINTENANCE MANUAL ® INTEL FALCON™ 8+ UAS The end of the boot process is marked by a triple beep emitted by the Intel ® Falcon™ 8+ UAS. Note: During boot up, the Intel ® Falcon™ 8+ UAS does not need to stand still. It can be moved - for example, it can be started from a moving boat.
Page 51: Motor Start
3. Left control Down 4. Start Motors START/STOP switch – 1 sec CAUTION: WHILE THE INTEL FALCON 8+ IS ON THE GROUND WITH RUNNING MOTORS, ALWAYS KEEP THE LEFT CONTROL STICK, WHICH CONTROLS THE HEIGHT THROTTLE, IN THE FULLY DOWNWARD POSITION TO AVOID ANY UNINTENTIONAL TAKE-OFF.
Page 52: Before Takeoff
Note: In Manual-Mode, the flight system will automatically descend when there is not enough thrust. Give at least 50% thrust to maintain height (depending on the attached payload). NORMAL PROCEDURES © 2017 Intel Corporation. All rights reserved. REV 00 APR 2017...
Page 53: Controlling The Intel
UAS in the horizontal pane are accessible with one single hand. Note: Note that all directional indications are always referring to the point of view of the Intel ® Falcon™ 8+ UAS. Depending on where the Intel ®...
Page 54: Descent
Right before touch-down – when the UAS is almost touching the ground – move the left control stick fully down to land the UAS. CAUTION: WHILE THE INTEL® FALCON™ 8+ UAS IS ON THE GROUND WITH RUNNING MOTORS, ALWAYS KEEP THE LEFT CONTROL STICK, WHICH CONTROLS THE HEIGHT, IN THE FULLY DOWNWARD POSITION TO AVOID ANY UNINTENTIONAL TAKE-OFF.
Page 55: After Landing
Engine Shutdown 1. Left control Down 2. START/STOP switch 1 second 3. Rotors Stopped spinning CAUTION: WHILE THE INTEL FALCON 8+ IS ON THE GROUND WITH RUNNING MOTORS, ALWAYS KEEP THE LEFT CONTROL STICK, WHICH CONTROLS HEIGHT, FULLY DOWNWARD POSITION AVOID UNINTENTIONAL TAKE-OFF.
Page 56: Post-Flight Check
In the transport case SECURING AIRCRAFT 1. Aircraft Condition Inspect 2. Aircraft and GCS Stowed in Case 3. Intel ® Powerpack™ Batteries Stowed in Case 4. Logbooks Complete NORMAL PROCEDURES © 2017 Intel Corporation. All rights reserved. REV 00 APR 2017...
Page 58: Section 5 Performance Planning
Enter if chosen / as required Loiter Points Enter chosen / as required Mission Termination Point Enter chosen / as required Altitudes Mission Duration Landing Area Identify and Program PERFORMANCE © 2017 Intel Corporation. All rights reserved. REV 00 APR 2017...
Page 59 Verify Entry Crew Brief Complete The Pilot will conduct a crew briefing to include all of the planned flight parameters as well as any notable field or operating conditions. PERFORMANCE © 2017 Intel Corporation. All rights reserved. REV 00 APR 2017...
Page 61 PAGE INTENTIONALLY LEFT BLANK...
Page 62: Section 6 Weight And Balance/Equipment List
AIRCRAFT WEIGHING PROCEDURES The Intel Falcon 8+ UA is designed to remain within manufacturers’ weigh and balance limits when using all authorized and approved payloads and components. Any alterations or substitutions are strictly prohibited and may void the warranty.
Page 64 13537 Intel Including Locknut Center Cross, Ready To Fly V1.0; Printed Circuit Boards 13739 Intel Cable Harnesses Screws Landing Foot 13748 Intel 13749 Intel WEIGHT / BALANCE / EQUIP © 2017 Intel Corporation. All rights reserved. REV 00 APR 2017...
Page 66 ITEM NOMENCLATURE NUMBER ASSY Payload, Camera Mount, Inspection V1.0; 13754 Panasonic Panasonic ZS50 FLIR Tau 2 640 Payload, Camera Gimbal, Inspection 13749 Intel V1.0 WEIGHT / BALANCE / EQUIP © 2017 Intel Corporation. All rights reserved. REV 00 APR 2017...
Page 67 ITEM NOMENCLATURE NUMBER ASSY Intel® Cockpit™ GCS Tablet V1.0; 13741 Intel Screws Intel® Cockpit™ GCS Housing, Ready To Use V1.0; 13742 Intel Electronic Components WEIGHT / BALANCE / EQUIP © 2017 Intel Corporation. All rights reserved. REV 00 APR 2017...
Page 70: Section 7 Aircraft And Systems Description
Falcon™ 8+ UAS can be launched in virtually any location where a minimal landing area is available. The system is designed for maximum portability and can be deployed within minutes. It is capable of flying for up to 26 minutes on two fully charged Intel ®...
Page 71: Central Unit
3) Retaining clip for the payload adapter 4) Cable tube, contains e.g. the cabling of the antennas. 5) Fan for the internal cooling behind the slots 6) Vibration dampers DESCRIPTION © 2017 Intel Corporation. All rights reserved. REV 00 APR 2017...
Page 72: Carbon Cross
5) Connector between Center Cross and Motor Rails 6) Landing Foot 7) Integrated video link antenna Each Motor Rail consists of four brushless Motor controllers seated within the carbon tube. DESCRIPTION © 2017 Intel Corporation. All rights reserved. REV 00 APR 2017...
Page 73: Electrical System
® Falcon™ 8+ UAS and Intel ® Cockpit GCS and combine efficiency with industrial safety standards. The Intel ® Powerpack™ Battery features automatic balancing, storage mode and charging. The intelligent Battery Management System (BMS) with a One-Button/Five-LEDs user interface makes everyday battery handling easy.
Page 74 The number of permanently lighted LEDs shows the progress of the charging process. If the next higher LED is blinking, this charging step is not yet finished. When the charging process is finished and the full capacity of the Intel ®...
Page 75 DAMAGE TO THE INTEL® POWERPACK™ BATTERY.  Charging will begin immediately indicated by blinking LEDs.  When charging is finished (all five LEDs are blinking simultaneously), unplug the Intel ® Powerpack™ Battery and the AC adapter. WARNING: DO NOT OVERCHARGE INTEL® POWERPACK™ BATTERY.
Page 76 (all LEDs off). Menu Option 2: Storage Mode When LED 2 is blinking, menu option 2 can be activated. When the button is pushed/held down for more than 2 secs, the Intel Powerpack™ Battery ® Storage Mode is activated. When this mode is activated all but one LEDs are on.
Page 77 The total number of charging cycles is shown via the LEDs in a binary system by powers of 2 from right to left multiplied by 10. Menu Option 4: Over All Capacity Menu option 4 shows the current possible amount of charge the Intel ® Powerpack™ Battery may hold when fully loaded as a percentage compared to the factory Intel ®...
Page 78 It can still be used for discharging one time as usual o It will not charge when connected to the power supply unit Error mode batteries must be returned to supplier For all other behavior of the LEDs contact an Intel ® Falcon™ 8+ UAS supplier.
Page 79: Lighting Systems - Exterior Lighting
Intel ® Powerpack™ Battery for disposal back to Intel. Disposing of this product correctly will be help to save valuable resources, and prevent any potential negative effects on human health and the environment, which could otherwise arise from inappropriate waste handling.
Page 80: Intel® Cockpit Ground Control Station
INTEL® COCKPIT GROUND CONTROL STATION The Intel ® Cockpit GCS is the main control hub for the Intel ® Falcon™ 8+ UAS and the attached payloads/cameras. It is designed to be carried and operated by one person and displays all relevant flight information.
Page 81: Intel Cockpit Gcs Control Unit
(B2) controls different camera functions depending on the attached payload 8) Four function buttons for the Status Display 9) RETURN TO HOME button 10) POWER on/off switch 11) Integrated shoulder harness holders DESCRIPTION © 2017 Intel Corporation. All rights reserved. REV 00 APR 2017...
Page 82 Other USB ports can be used to connect USB sticks with preplanned flight  missions to be imported. HDMI Port A headphone port (mini jack) is located on the lower right hand side of the Intel ® Cockpit GCS Before placing headphones or earphones near the ear 1.
Page 83: Overview Of The Status Display Controls
® Cockpit GCS. 7.2.2 Overview of the Status Display Controls The Status Display shows all relevant information for flying. It is built into the Intel ® Cockpit GCS control unit. The Status Display shows the current settings and allows the operator to adjust specific functions of the Intel ®...
Page 84 INTEL FALCON™ 8+ UAS Touch Screen The Intel® based Windows® touch screen has a resolution of 1920 X 1200 pixels and an 8.3 inch screen. It is directly mounted on the remote unit of the Intel ® Cockpit GCS and should not be removed.
Page 85 The button in the lower left corner, opens a window providing information about the software (version, available updates, etc.). In the left top corner, there are two buttons: DESCRIPTION © 2017 Intel Corporation. All rights reserved. REV 00 APR 2017...
Page 86: Normal Operation: Preparing The Intel
1. Open the lid of the battery compartment and slide the Intel ® Powerpack™ Battery with the colored label facing downwards into the battery compartment. Slide it all the way in until it is stopped and flush with the end of the slot. The Intel ® Powerpack™ Battery feeds the Intel ®...
Page 87: Flight Modes
 Height-Mode  Manual-Mode Note: Flying in GPS-Mode is easiest as it provides the highest level of automation. The flight modes can be selected with the two switches on the upper right of the Intel ® Cockpit GCS.  When the button GPS is pushed and is lit, GPS-Mode is active ...
Page 88 Ascend rate is limited to 7 mph (3 m/s).  Descend rate is limited to 7 mph (3 m/s). CAUTION: AVOID FULL THROTTLE INPUTS IN HEIGHT-MODE AS THE INTEL® FALCON™ 8+ UAS CAN BE OVERSTRESSED IN CERTAIN SITUATIONS, E.G. FLYING ABRUPT MANEUVERS WITH A LOW BATTERY.
Page 89: Camera Controls
Intel ® Falcon™ 8+ UAS. o Roll and pitch angles are limited to 50°. o The direction and the speed of the Intel Falcon™ 8+ UAS are influenced by the ® wind direction and speed. WARNING: MANUAL-MODE IS FOR EXPERTS ONLY.
Page 90: Special Functions
® INTEL FALCON™ 8+ UAS 5) Right Rocker-Switch, #5, changes its function depending on the used camera. 6) Control Stick, #6, turns the right control stick controls the yaw axis of the Intel ® Falcon™ 8+ UAS. 7) Push Button #7 is the Status Display and related control buttons 8) Push Buttons #8 (ESC, LEFT, RIGHT, ENT), depending on the payload, offer additional options that can be accessed via the Status Display.
Page 91 FT: flight time o Dist: distance from home position  The COI flight can be interrupted by giving a strong control stick command on the Intel ® Cockpit GCS or by pushing the ESC button of the Status Display.
Page 92 ® Falcon™ 8+ UAS can take images at predefined positions, optimized for later stitching the images into one, large panorama shot. The speed of the Intel ® Falcon™ 8+ UAS is set automatically to always have 2 seconds in between images. Any photo editing software with panorama stitching functionality, or specialized panorama software, may be used to do the image post processing.
Page 93 360° turn around the yaw axis, with one fixed tilt angle of the camera. To do a cylindrical panorama:  Do all necessary camera adjustments, take off and fly the Intel ® Falcon™ 8+ UAS to the desired position.
Page 94 Follow these steps to do a cylindrical panorama:  Do all necessary camera adjustments, take off and fly the Intel ® Falcon™ 8+ UAS to the desired position.
Page 95  Use the arrow LEFT button to activate START! and confirm by pushing ENT.  The camera will be tilted downwards and the Intel ® Falcon™ 8+ UAS will start doing multiple 360° turns while slowly tilting the camera further upwards, until the spherical panorama is completed.
Page 96 77 102 128 154 180 205 231 257 282 308 334 Row 11 98 130 163 196 229 261 294 327 Row 12 51 102 154 205 257 308 Row 13 Total: 154 images DESCRIPTION © 2017 Intel Corporation. All rights reserved. REV 00 APR 2017...
Page 97 Quick Surveying Assistant This function is available as part of the Survey Package. Survey Assist offers a quick and easy way to do a mapping flight over a rectangular area, directly from the Intel ® Cockpit GCS without any prior planning on a computer. To do so, the Intel ®...
Page 98  Side Overlap: Define the percentage of image overlap between the lines (cross track).  Select Cam: Select camera/lens combination attached to the Intel Falcon™ 8+ UAS. The ® most commonly used cameras are available as a preset. ...
Page 99 No of Lines: Define the number of lines which shall be flown. The resulting area, which will be covered by the images, is calculated and displayed in ha (hectare). The estimated required flight time to perform the flight is also presented. DESCRIPTION © 2017 Intel Corporation. All rights reserved. REV 00 APR 2017...
Page 100 The AscTec Navigator Software enables planning and performing complex flight patterns for remote surveying applications. Pre-planned AscTec Navigator Software flight missions are exported to an USB stick, which is plugged into one of the USB ports of the Intel ®...
Page 101: Camera Mount And Gimbal
This flight plan can be loaded and executed using the NAVIGATOR function of the Intel ® Cockpit GCS application on the touchscreen tablet. At each waypoint an image is triggered, and the current GPS position is stored in the Intel ®...
Page 102: Camera Mount Exchange
Falcon™ 8+ UAS.  Make sure that the ball of the ball link connector of the roll servo is fixed in the respective slot in the adapter when the camera mount is fixed onto the Intel ® Falcon™ 8+ UAS.
Page 103: Inspection Payload
The SD card of the camera is inserted next to the battery. A separate charger for the Panasonic Lumix batteries is supplied with the payload. DESCRIPTION © 2017 Intel Corporation. All rights reserved. REV 00 APR 2017...
Page 104 MAINTENANCE MANUAL ® INTEL FALCON™ 8+ UAS The FLIR Tau 2 640 camera is powered by the Intel ® Falcon™ 8+ UAS battery to save weight, and does not need to be switched on or off. The micro SD card of the FLIR Tau is inserted at the side of the camera, with the contacts of the micro SD facing towards the camera lens.
Page 105 Program Inspection Payload by the Status Display Push the ENT button of the Status Display Intel ® Cockpit GCS to enter the menu. Navigate to Camera Options. THE FOLLOWING OPTIONS ARE AVAILABLE FOR THE INSPECTION PAYLOAD ZS50: Switches the live image preview on the touch screen between the...
Page 106 FALCON™ 8+ UAS Inspection Payload Control by the Intel ® Cockpit GCS The Inspection Payload ZS50 can be operated by using the functional elements of the Intel ® Cockpit GCS. Refer to Section 7.3.6 Camera Controls for specific button functions. Additionally: ...
Page 107: Sony Alpha 7R Full Frame Camera
3) C2: provides quick access to the Focus Mode 4) WB: provides quick access to White Balance. ISO can be quickly accessed by turning the control wheel in the back of the camera. DESCRIPTION © 2017 Intel Corporation. All rights reserved. REV 00 APR 2017...
Page 108 Refer to the camera manual for further details. Program Sony Alpha 7R Full Frame Camera by the Status Display Push the ENT button of the status of the Intel Cockpit GCS. Press display to enter the menu. ® Navigate to Camera Options.
Page 109 Sony Alpha 7R Full Frame Camera Control by the Intel ® Cockpit GCS The Sony Alpha 7R can be operated by using the functional elements of the Intel ® Cockpit GCS. Refer to Section 7.3.6 Camera Controls for specific button functions.
Page 112: Section 8 Handling, Servicing And Maintenance
FALCON™ 8+ UAS OWNER ADVISORIES ® Intel Product Advisories are posted on the internet and available at no charge to inform owners about mandatory and/or beneficial aircraft service requirements and product changes. Copies of the service bulletins are available from Intel approved Depot Stations and Intel Customer Service.
Page 114: Initial Set Up
® Falcon™ 8+ UAS and Intel ® Cockpit GCS.  Set the system date and time on the touch screen Tablet of the Intel Cockpit GCS. ®  Perform a payload and compass calibration with every payload. See Section 4.3.2.
Page 115: Initial Setup Of The Intel Cockpit Gcs Tablet
1) Push the ENT button of the Status Display. The screen to enter the serial number (5- digit serial number of the Intel ® Falcon™ 8+ UAS, printed on the top side of the Intel ® Falcon™ 8+ UAS above the battery compartment) will appear. The first digit is highlighted.
Page 116: Remote Pilot Conducted Preventive Maintenance
 Onboard navigation and communication data links;  Any equipment, such as a camera, is securely attached;  Spinning propellers for any imbalance or irregular operation. SERVICE / MAINTENANCE © 2017 Intel Corporation. All rights reserved. REV 00 APR 2017...
Page 117: Life-Limited Parts
Assess the need and extent of repairs sparking, etc.) that may be needed for continued safe flight operations, aircraft performance Further Action: characteristics, and flight duration. Requires Repair from Service Depot. SERVICE / MAINTENANCE © 2017 Intel Corporation. All rights reserved. REV 00 APR 2017...
Page 118 Requires Repair from flyaway. Service Depot.  Assess the need and extent of repairs that may be needed for continued safe flight operations. SERVICE / MAINTENANCE © 2017 Intel Corporation. All rights reserved. REV 00 APR 2017...
Page 119: Operational Checks
CONDITION ACTION RESOLUTION  Further inspect to determine integrity Remote Pilot Action: of the Intel® Powerpack™ Battery as a Use commercially reliable power source. Inspect to available canned ensure both battery compartments are compressed air to fully operational. remove dirt and ...
Page 120 FALCON™ 8+ UAS All Normal Checklist actions apply to Operational Check flights. If there are unknown visible damages from the last transport, Is the transport case free take special care during the check of the complete Intel ® Falcon™ of visible damage? 8+ UAS.
Page 121: Camera Horizon
Using the Intel ® Cockpit GCS, select Link Loss Procedure if required.  Push the left control stick of the Intel ® Cockpit GCS fully upwards and hold it.  While holding the left control stick fully upwards, use the right control stick to adjust the camera.
Page 122: Field Repair
Depending on the applied force, the Propeller should make several turns.  Check the orientation of the Propeller once more, and compare the movement with the other Propellers. SERVICE / MAINTENANCE © 2017 Intel Corporation. All rights reserved. REV 00 APR 2017...
Page 123 Remove the Motor Rail from the Center Cross by pushing the plugs of the Motor Rail up. CAUTION: ROTATING THE MOTOR RAILS TOO MUCH CAN CAUSE THE CONNECTORS TO BREAK SERVICE / MAINTENANCE © 2017 Intel Corporation. All rights reserved. REV 00 APR 2017...
Page 124 Apply a thread locking agent to the screws.  Using a T6 Torx screwdriver, screw in to two Motor Rail screws.  Ensure the Propellers rotate in the correct direction. SERVICE / MAINTENANCE © 2017 Intel Corporation. All rights reserved. REV 00 APR 2017...
Page 125: Ground Handling
CAUTION: THE INTEL® FALCON™ 8+ UAS AND INTEL® COCKPIT GCS SHOULD BE TRANSPORTED FULLY ASSEMBLED. CAUTION: WHEN SHIPPING THE INTEL® FALCON™ 8+ UAS IN THE TRANSPORT CASE WITH A MOUNTED PAYLOAD, THE FOAM INLET OF THE PAYLOAD CASE MUST BE USED TO AVOID DAMAGES DURING TRANSPORT.
Page 126: Packing
FALCON™ 8+ UAS 8.9.2 Packing Intel ® Falcon™ 8+ UAS Case This case is used for all necessary parts of the Intel ® Falcon™ 8+ UAS. Following the numbers, this case contains: 1) Intel ® Falcon™ 8+ UAS without payload 2) Power supply units for charging the Intel Power Packs 3) Space for accessories, e.g.
Page 127 This ensures the touch screen is extra-protected against scratches during transportation. 2) Additional storage space 3) Additional storage space (e.g. for an extra power supply) Not shown: Reflective safety vest under the sunshade protected touch screen. SERVICE / MAINTENANCE © 2017 Intel Corporation. All rights reserved. REV 00 APR 2017...
Page 128 The foam bolster cover on top of the payload (not shown) must be used to secure the payload when it is transported mounted on the Intel ® Falcon™ 8+ UAS in the case.
Page 129 3) Use the four tie straps tapes to secure the Intel ® Falcon™ 8+ UAS inside the backpack. The tie straps must be very tight so that the system is "lifted" up and away from the Intel ® Cockpit GCS.
Page 130: Unpacking
Intel cannot assume any liability for failures to comply with these warnings and safety guidelines. By purchasing this battery, the customer assumes all risks associated with lithium batteries.
Page 131 Check the Intel ® Powerpack™ Battery voltage after charging. Voltage is shown on the status display and by the LEDs and on the Intel Cockpit GCS touch screen. The voltage for a 4-cell ® battery should fall between 16.4 V – 16.6 V.
Page 132: Cleaning And Care
A small, soft paintbrush (dry) may also be helpful for cleaning.  For cleaning (especially the Motors) and drying canned compressed air can also be used. CAUTION: IF COMPRESSED AIR IS USED FOR CLEANING THE INTEL ® FALCON™ 8+ UAS, IT IS MANDATORY TO HOLD/FIX THE PROPELLERS DURING THE BLOWING OUT PROCEDURE.
Page 133: Sony Alpha 7R Full Frame Camera General Care
Falcon™ 8+ UAS battery to save weight. When the system is switched off always switch off the camera first and wait for 10 seconds to enable the camera to fully power down and store all images and settings. Only then switch off the Intel Falcon™...
Page 136: Section 9 Supplements
This section shall contain the appropriate Supplements necessary to safely and efficiently operate the aircraft when equipped with the various optional system and equipment not provided with the standard aircraft. Supplements may be prepared by the Manual producer. SUPPLEMENTS © 2017 Intel Corporation. All rights reserved. REV 00 APR 2017...
Page 137 REGISTRATION NO._____________________ This supplement must be inserted into Section 9 of the Pilot's Operating Handbook and Aircraft Flight Manual when the Independent Camera Control (ICC) is installed. © 2017 Intel Corporation. All rights reserved. INTEL CORPORATION 2200 MISSION COLLEGE BLVD...
Page 138: Supplement 1: Independent Camera Control
There is no change to the aircraft performance when the Independent Camera Control (ICC) is used. SECTION 6- WEIGHT AND BALANCE There is no change to the aircraft weight and balance when the Independent Camera Control (ICC) is used. SUPPLEMENTS © 2017 Intel Corporation. All rights reserved. REV 00 APR 2017...
Page 139: Section 7- Aircraft And Systems Description
SECTION 7- AIRCRAFT AND SYSTEMS DESCRIPTION The Independent Camera Control (ICC) allows a camera operator to control the main camera functions from a gamepad, which is connected to the Intel Cockpit GCS via a port located on ® the back of the Intel ®...
Page 140: Section 8- Handling, Servicing And Maintenance
There is no change to the aircraft handling, servicing and maintenance when the Independent Camera Control (ICC) is used. SECTION 10- SAFETY There is no change to the aircraft safety when the Independent Camera Control (ICC) is used. SUPPLEMENTS © 2017 Intel Corporation. All rights reserved. REV 00 APR 2017...
Page 142: Safety
Intended Use This product is an unmanned aircraft system (UAS) intended for commercial use only. It is not intended for consumer or recreational use. Users must read and understand all documentation before using the Intel ® Falcon™ 8+ UAS. By using the Intel ®...
Page 143 Intel recommends every Remote Pilot receive training on the proper operation of the Intel® Falcon™ 8+ UAS in all flight modes and to maintain the Intel® Falcon™ 8+ UAS in a safe and airworthy condition is mandatory. For training on your UAS, please contact your dealer from which you purchased the UAS or contact Intel, if you purchased the UAS directly from Intel.
Page 144 Therefore a Remote Pilot must have the training and ability to fly the Intel® Falcon™ 8+ UAS in Height-Mode in any situation. Only operate in these environment with sufficient training! ...
Page 145: Weather
This information is not designed to provide, nor shall it be deemed to constitute, any legal advice or include any kind of warranty regarding the usability of the UAS. Please contact legal counsel for any binding advice on the use of the Intel® Falcon™ 8+ UAS in the applicable jurisdiction.
Page 146: Accident/Incident Reporting
MAINTENANCE MANUAL ® INTEL FALCON™ 8+ UAS GPS stability and/or the magnetic field sensor. The Intel ® Falcon™ 8+ UAS is designed to compensate these errors in most cases, but the function is not guaranteed. Takeoff/Launch and Landing Operations The safety of personnel working in or around the takeoff/launch and landing site is the single largest concern.

Intel FALCON 8+ Flight Manual

Record of Revision

Table of Contents

Section 1 General

Section 2 Limitations

Intelfalcon™ 8+ Uas

Maintenance Manual

Section 3 Emergency Procedures

Section 4 Normal Procedures

Section 5 Performance Planning

Section 6 Weight and Balance/Equipment List

Section 7 Aircraft and Systems Description

Intelfalcon™ 8+ Uas

Maintenance Manual

SECTION 8 HANDLING, SERVICING and MAINTENANCE

Section 9 Supplements

Supplement 1: Independent Camera Control

Safety

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Summary of Contents for Intel FALCON 8+

Table of Contents