UAS OSC Volume 2

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Operator ID:

 

UAS Operating Safety Case
Volume 2 - UAS Description:

 

Document reference number:

 

Document version and date:

 

Amendment record

Amendment Number

Date

Amended by

Details of changes

 

 

 

 

CAP722A Table 6


Aircraft and systems description

UAS Model

Mavic 2 Enterprise Advanced

UAS design & manufaturing organisations

DJI

UAS physical characteristics

Empty Mass

Maximum Take-Off Mass (MTOM)

Takeoff Weight:
909g

Max Takeoff Weight:
1100g

Dimensions for Rotorcraft / Multirotor

Length of aircraft body

Dimensions:
Folded: 214 x 91 x 84mm
Unfolded: 322 x 242 x 84mm
Unfolded+Spotlight: 322 x 242 x 114mm
Unfolded+Beacon: 322 x 242 x 101mm
Unfolded+Speaker: 322 x 242 x 140mm
Unfolded+RTK Module: 322x242x125mm

Diagonal Distance:
354 mm

Width of aircraft body

Height of aircraft body

Propeller Configuration

Propeller Dimensions

Sound power level

Any other relevant information

CAP722A Table 7

UAS performance characteristics

Maximum airspeed

Max Speed (near sea level, no wind):
72 kph (S-mode, without wind)
50 kph (P-mode, without wind)

Minimum airspeed to maintain safe flight

Normal/typical operating height

Maximum operating height

Max Service Ceiling Above Sea Level:
6000 m

Maximum flight time during normal operation

Max Flight Time:
31 min (measured while flying at 25 kph in windless conditions)
28 min (RTK module attached)
29 min (with beacon turned on)
30 min (with beacon turned off)
24 min (with spotlight turned on)
28 min (with spotlight turned off)
27 min (with speaker turned on)
28 min (with speaker turned off)

Maximum flight time on an ISA day at cruising speed at normal/typical operating height.

Maximum flight range on an ISA day (normal and emergency conditions)

Glide distances

Maximum radio range of the C2 Link

Max Transmission Distance (unobstructed, free of interference):
2.400 - 2.483 GHz; 5.725 - 5.850 GHz
FCC: 10000m
CE: 6000m
SRRC: 6000m
MIC: 6000m

CAP722A Table 8

UAS environmental limitations

Wind speed limits

Max Wind Speed Resistance:
10 m/s (scale 5)

Turbulence restrictions

Precipitation limits

OAT limits

Operating Temperature:
-10 Deg. to 40 Deg. C

In-flight icing condition limits

Any other relevant information

CAP722A Table 9

Construction

Type of material

Material characteristics or properties

Any other relevant information

CAP722A Table 10

Electrical power system

Batteries:

Battery type, model and manufacturer

Capacity[1]:
3850 mAh

Battery Type:
LiPo

Quantity

Arrangement

Generator:

Generator type, model and manufacturer

Specification

Electrical loads

Voltage:
15.4V

Energy:
59.29 Wh

Electrical load shedding functionality

Power supply redundancy

Procedures to charge and discharge batteries.

Safety provisions with regards to hazards inherent to high-voltage storage devices:

Procedures in place for safe handling by any person who may come into contact with high-voltage storage devices

Means of identifying high-voltage storage

Safety provisions for any person discovering the UA following an accident.

Procedures and safety provisions to mitigate the risk of battery thermal runaway.

Procedures for monitoring high-voltage storage devices.

HMI:

Information indicated to the remote pilot.

Alert messages indicated to the remote pilot.

Any other relevant information

Net Weight:
297g

Charging Time:
90 mins

Charging Temperature:
5 Deg.C - 40 Deg.C

Operating Temperature Range:
-10 Deg.C - 40 Deg.C

Heating Methods:
Manual Heating, Auto Heating

Heating Temperature:
-20 Deg.C - 6 Deg.C

Heating duration:
500s (Max)

Heating Power:
55W (Max)

CAP722A Table 11

Propulsion system

Propulsion type

Engines:

Type, model and manufacturer

Propeller type, model and manufacturer

Quantity

Arrangement

Power output

Propeller guards

In-flight restart functionality

Performance monitoring

Health monitoring

Safety features and redundancy in the system that allow maintaining flight after a failure or degradation has occurred in the propulsion system.

Fuel-powered propulsion system – Safety features to mitigate the risk of engine loss when the following hazards occur:

Fuel starvation

Fuel contamination

Failed signal input from the control station

Engine controller failure

Indication to the remote pilot

Electric-powered propulsion system:

Power source and supply management with regards to other systems in the UA

Redundant power sources

Maximum continuous power output of the motor

Maximum peak power output of the motor

Electrical distribution architecture

Electrical load shedding functionality

HMI:

Information indicated to the remote pilot.

Alert messages indicated to the remote pilot.

Any other relevant information

CAP722A Table 12

Fuel system

Fuel type

Safety provisions with regards to hazardous substances within the fuel system:

List of hazardous substances and their characteristics.

Procedures in place for safe handling of the UA by any person who may come into contact with the hazardous substances.

Means of identifying the hazardous substances.

Safety provisions for any person discovering the UA following an accident.

HMI:

Information indicated to the remote pilot.

Alert messages indicated to the remote pilot.

Any other relevant information

CAP722A Table 13

Flight Controls system

Design and operation of flight control units, surfaces, actuators, control linkages, etc.

Flight controller:

Type, model and manufacturer

Functions

Flight modes available

Automatic functions:

Take-off and landing

Stabilisation

Autopilot

Return to home

If functions are provided by COTS equipment, provide type, model and manufacturer.

Safety features and redundancy in the system which allow maintaining flight after a failure or degradation of the flight control system, including indication to the remote pilot.

HMI:

Information indicated to the remote pilot.

Alert messages indicated to the remote pilot.

Any other relevant information

CAP722A Table 14

Navigation

Sensors

Type, model and manufacturer

GNSS:
GPS+GLONASS

Quantity

Telemetry links

Method to determine current position.

Method to navigate to intended destination.

Automatic/automated navigation functions

Geo-awareness functions

RTK Positioning Precision:
In RTK FIX
1cm+1ppm (Horizontal)
1.5cm+1 ppm (Vertical)

Containment functions

Safety features and redundancy in the system which allow maintaining flight after a failure or degradation has occurred in the navigation system:

Backup means of navigation

Detection of and response to loss of primary means and secondary means of navigation.

Indication to the remote pilot

HMI:

Information indicated to the remote pilot.

Alert messages indicated to the remote pilot.

Any other relevant information

CAP722A Table 15

Detect and Avoid (DAA) systems

DAA system functions

Forward:
Precision Measurement Range: 0.5 - 20 m
Detectable Range: 20 - 40 m
Effective Sensing Speed: <= 14m/s
FOV: Horizontal: 40 Deg., Vertical: 70 Deg.

Backward:
Precision Measurement Range: 0.5 - 16 m
Detectable Range: 16 - 32 m
Effective Sensing Speed: <= 12m/s
FOV: Horizontal: 60 Deg., Vertical: 77 Deg.

Downward:
Precision Measurement Range: 0.5 -11m
Detectable Range: 11-22 m

Upward:
Precision Measurement Range: 0.1-8 m

Operating Environment:
Forward, Backward and Sides:
Surface with clear pattern and adequate lighting
(lux > 15)
Upward: Detects diffuse reflective surfaces(>20%)
(walls, trees, people, etc.)
Downward: Surface with clear pattern and adequate lighting
(lux > 15)Detects diffuse reflective surfaces (>20%)
(walls, trees, people, etc.)

Sensing System:
Omnidirectional Obstacle Sensing[2]

Sides:
Precision Measurement Range: 0.5 - 10 m
Effective Sensing Speed: <= 8m/s
FOV: Horizontal: 80 Deg., Vertical: 65 Deg.

Devices used

Technology used

Interface between the DAA system and the flight control computer

Limitations of the DAA system

Evidence of equipment qualification and approval.

DAA event sequence:

Level of automation

Actions required by the remote pilot

Means to verify normal system operation.

HMI:

Information indicated to the remote pilot.

Alert messages indicated to the remote pilot.

Any other relevant information

CAP722A Table 16

Other avionics systems

 

Command Unit (CU)

Power sources, supply management and redundancy.

Built-in battery:
Type: 18650 Li-Po （5000 mAh @ 7.2 V)
Charging Mode: Charged with USB charger at 12V/2A
Rated Power 15 W
Charging time: 2 hr (with a USB charger at 12V/2A)

Intelligent Flight Battery:
Main Link: 17.6V ⎓ 3.41A or 17.0V⎓3.53A
USB: 5.0 V ⎓ 2.0 A

Radio signal:

Determination of the signal strength and health value.

Threshold values which represent a critically degraded signal.

Control handover between two CUs

Safety features to mitigate the risk of inadvertent command activation:

List of critical commands

Mitigation means

Safety features to mitigate the risk of display or HMI lock-up.

Safety features to maintain flight-critical processing when multiple programs are running concurrently.

HMI:

Information indicated to the remote pilot.

Radio signal strength and/or health indication to the remote pilot.

Alert messages indicated to the remote pilot.

Any other relevant information

Battery Life:
Built-in Battery Approx. 2.5 hr

Operating Temperature:
-20 Deg. C - 40 Deg. C

CAP722A Table 17

Command an Control (C2) link

RLOS

BRLOS

Antennas:

Type, model and manufacturer

Locations on the UAS

Transceivers / Modems:

Power levels

Transmitter Power (EIRP):
2.400 - 2.4835 GHz
FCC: <=26 dBm；
CE: <=20 dBm；
SRRC: <=20 dBm;
MIC: <=20 dBm
5.725 - 5.850 GHz
FCC: <=26 dBm;
CE: <=14 dBm;
SRRC: <=26 dBm

Transmission Power (EIRP):
2.400-2.4835 GHz:
25.5 dBm（FCC) ；18.5 dBm（CE) 19 dBm（SRRC) ；18.5 dBm（MIC)
5.725-5.850 GHz:
25.5 dBm（FCC) ；12.5 dBm（CE) 18.5 dBm（SRRC)

Transmission schemes

Operating frequencies

Details of frequency spectrum approvals

Operating Frequency:
2.400-2.4835 GHz;
5.725-5.850 GHz

Operating Frequency:
2.400 - 2.483 GHz;
5.725 - 5.850 GHz

Maximum power output/range

Type of signal processing

Datalink margin in terms of the overall link bandwidth at the maximum anticipated distance from the CU.

Operational C2 link management:

Frequency switchovers

Contingency situations

Third party link service provider

Radio signal:

Determination of the signal strength and health value

Threshold values which represent a critically degraded signal.

Minimum and average assured data rates

Minimum and average assured latencies

Design features and procedures to maintain availability, continuity, and integrity of the datalink:

RF or other interference

Flight beyond communications range

Antenna masking

Loss of CU functionality

Loss of UA functionality

Atmospheric attenuation

Safety features to mitigate the risk of loss of C2 link:

C2 links redundancy

Automatic triggering of an emergency recovery function

Automatic return to home

Safety features to mitigate the risk of harmful interference.

HMI:

Information indicated to the remote pilot.

Radio signal strength and/or health indication to the remote pilot.

Alert messages indicated to the remote pilot.

Any other relevant information

CAP722A Table 18

Communications

Antennas:

Type, model and manufacturer

Locations on the UAS

Communication method:

VHF

GSM network

Satellite

Safety features to mitigate the loss of communication function:

Primary communication means

Secondary / back-up communication means

HMI:

Information indicated to the remote pilot.

Radio signal strength and/or health indication to the remote pilot.

Alert messages indicated to the remote pilot.

Any other relevant information

CAP722A Table 19

Take-off and landing mechanisms

Wheels, skids, rails, launchers, etc.

If various mechanisms can be fitted:

Primary mechanism

Secondary mechanisms

Operational conditions/requirements for each mechanism.

Any other relevant information

CAP722A Table 20

Emergency recovery and safety systems

Mode of operation

Safety features which mitigate the risk of loss of control or situational awareness.

Means to verify normal system operation.

HMI:

Information indicated to the remote pilot.

Alert messages indicated to the remote pilot.

Any other relevant information

CAP722A Table 21

External lighting

Type, model and manufacturer

Locations on the UA

Colour

Operation

Operating modes

Purpose

HMI:

Information indicated to the remote pilot.

Alert messages indicated to the remote pilot.

Any other relevant information

CAP722A Table 22

Payload

Types

Mass

Interfaces with the UA:

Mechanical interface

Electrical interface

Connections:
Micro USB Port

Connections:
Micro USB Port

Connections:
Micro USB Port

Data interface

Release mechanism

Any other interface

Procedures to install the payload onto the UA.

Effects of the payload on the UA

Sensors

Sensor:
Uncooled VOx Microbolometer

Sensor:
1/2" CMOS, Effective Pixels: 48 M

Safety features to mitigate the risk of the payload affecting the flight of the UA:

Effects on aerodynamics

Effects of electro-magnetic interference.

Effects of electrical power and / or data connection failures on the UAS.

Effects of complete detachment of the payload from the UA (either caused by a failure or through intentional lowering / dropping of the payload).

Effects of partial detachment of the payload from the UA.

Distraction of the remote pilot generated by the payload during flight.

Procedures to verify the attachment points to the UA.

Procedures to verify the UA MTOM and CG location.

Procedures to detect and mitigate any failure of the payload in flight.

Safety provisions with regards to hazards inherent to the payload

Procedures in place for safe handling of the payload.

Means of identifying hazards.

HMI:

Information indicated to the remote pilot.

Alert messages indicated to the remote pilot.

Any other relevant information

Dimensions:
69 mm x 69 mm x 59mm

CAP722A Table 23

Ground support equipment

UAS launch and recovery systems

Power sources

Transportation equipment

Backup or emergency equipment

Procedures to transport UA, CU, battery/fuel, and other equipment between operation sites and from the loading/off-loading area to the take-off/landing area.

Storage of ground support equipment.

Suitability of the ground support equipment and transportation method with regards to the UAS components’ fragility, sensitivity or inherent hazards.

Ground support equipment standards

Ground support equipment manufacturer's recommendations.

Any other relevant information

CAP722A Table 24

Maintenance

Maintenance manual:

Structure

Maintenance procedures:

Inspections

Overhaul

Repairs

Assurance of repair procedures

Batteries maintenance during storage periods

Origin of each procedure

Maintenance schedules

Procedures to record maintenance that has been carried out.

Storage of maintenance records

Staff qualification and levels of approval.

Procedures to use the manual by the Maintenance staff

Configuration control

Any other relevant information

CAP722A Table 25

Spare parts procurement

Sources of procurement

Process to confirm the suitability of the part.

Any other relevant information

CAP722A Table 26

Change Management and modifications to the system

Hardware, software, and firmware version control

Modification standards

Modification records storage

Safety assessment associated with the modification

Any other relevant information

CAP722A Table 27


Safety features of the UAS

Step 1 – Identify the main functions of the UAS.

 

Step 2 – Identify the sub-functions.

 

Step 3 – Consider the ways each function may fail.

 

Step 4 – Identify the failure conditions.

 

Step 5 – Select those failure conditions that may lead to mid-air collision or harm to uninvolved people on the ground. (Identified Hazard)

 

Step 6 – Assurance

 

Step 7 – Describe the consequence of the failure condition.

 

Step 8 – Describe the failure modes. (Unmitigated Failures)

 

Step 9 – Identify the single points of failure.

 

Step 10 – Describe the risk mitigation means.

 

CAP722A Table 28


ANNEX - Manufacturer supplied data forDJI Mavic 2 Enterprise Advanced

Aircraft

Takeoff Weight909g
Max Takeoff Weight1100g
DimensionsFolded: 214 x 91 x 84mm
Unfolded: 322 x 242 x 84mm
Unfolded+Spotlight: 322 x 242 x 114mm
Unfolded+Beacon: 322 x 242 x 101mm
Unfolded+Speaker: 322 x 242 x 140mm
Unfolded+RTK Module: 322x242x125mm
Diagonal Distance354 mm
Max Ascent Speed6 m/s (S-mode)
5 m/s (P-mode)
4 m/s (S-mode with accessories)
4 m/s (P-mode with accessories)
Max Descent SpeedDescend Vertically
5 m/s (S-mode)
4 m/s (P-mode)
Tilt
7 m/s (S-mode)
4 m/s (P-mode)
Max Speed (near sea level, no wind)72 kph (S-mode, without wind)
50 kph (P-mode, without wind)
Max Service Ceiling Above Sea Level6000 m
Max Flight Time31 min (measured while flying at 25 kph in windless conditions)
28 min (RTK module attached)
29 min (with beacon turned on)
30 min (with beacon turned off)
24 min (with spotlight turned on)
28 min (with spotlight turned off)
27 min (with speaker turned on)
28 min (with speaker turned off)
Max Wind Speed Resistance10 m/s (scale 5)
Max Tilt Angle35 Deg.(S-mode, with remote controller)
25 Deg.(P-mode)
Max Angular Velocity200 Deg./s (S-mode)
100 Deg./s (P-mode)
Operating Temperature-10 Deg. to 40 Deg. C
GNSSGPS+GLONASS
Hovering Accuracy RangeVertical:
± 0.1 m (with RTK)
± 0.1 m (with Vision Positioning)
± 0.5 m (with GPS Positioning)
Horizontal:
± 0.1 m (with RTK)
± 0.3 m (with Vision Positioning)
± 1.5 m (with GPS Positioning)
Operating Frequency2.400-2.4835 GHz;
5.725-5.850 GHz
Transmitter Power (EIRP)2.400 - 2.4835 GHz
FCC: <=26 dBm；
CE: <=20 dBm；
SRRC: <=20 dBm;
MIC: <=20 dBm
5.725 - 5.850 GHz
FCC: <=26 dBm;
CE: <=14 dBm;
SRRC: <=26 dBm
Internal Storage24 GB

M2EA Thermal Camera

SensorUncooled VOx Microbolometer
Focal LengthApprox. 9mm
35 mm format equivalent: Approx. 38mm
Sensor Resolution640 x 512 @30Hz
Accuracy of Thermal TemperatureMeasurement: ±2 Deg.C or ±2%, whichever is greater.
Scene Range-20 Deg.C to 150 Deg.C (High Gain)
-20 Deg.C to 450 Deg.C (Low Gain)
Digital Zoom16 x
Pixel Pitch12 μm
Spectral Band8-14 μm
Photo FormatR-JPEG
Video FormatMP4
Metering MethodSpot Meter, Area Measurement
FFCAuto/Manual

M2EA Visual Camera

Sensor1/2" CMOS, Effective Pixels: 48 M
LensFOV: 84 Deg.
35 mm format equivalent: 24 mm
Aperture: f/2.8
Focus: 1 m to ∞
ISO RangeVideo: 100-12800 (auto)
Photos: 100-1600 (auto)
Digital Zoom32 x
Max Image Size8000 x 6000
Still Photography ModesSingle shotInterval: 2/3/5/7/10/15/20/30/60 s
Panorama: Sphere
Video Resolution3840 x 2160@30fps
1920 x 1080@30fps
Photo FormatJPEG
Video FormatMP4

Gimbal

Mechanical RangeTilt: -135 Deg.- +45 Deg.
Pan: -100 Deg.- +100 Deg.
Controllable RangeTilt: -90 Deg.- +30 Deg.
Pan: -75 Deg.- +75 Deg.
Stabilization3-axis (tilt, roll, pan)
Max Control Speed (tilt)120 Deg./s
Angular Vibration Range±0.005 Deg.

Sensing System

Sensing SystemOmnidirectional Obstacle Sensing[2]
ForwardPrecision Measurement Range: 0.5 - 20 m
Detectable Range: 20 - 40 m
Effective Sensing Speed: <= 14m/s
FOV: Horizontal: 40 Deg., Vertical: 70 Deg.
BackwardPrecision Measurement Range: 0.5 - 16 m
Detectable Range: 16 - 32 m
Effective Sensing Speed: <= 12m/s
FOV: Horizontal: 60 Deg., Vertical: 77 Deg.
UpwardPrecision Measurement Range: 0.1-8 m
DownwardPrecision Measurement Range: 0.5 -11m
Detectable Range: 11-22 m
SidesPrecision Measurement Range: 0.5 - 10 m
Effective Sensing Speed: <= 8m/s
FOV: Horizontal: 80 Deg., Vertical: 65 Deg.
Operating EnvironmentForward, Backward and Sides:
Surface with clear pattern and adequate lighting
(lux > 15)
Upward: Detects diffuse reflective surfaces(>20%)
(walls, trees, people, etc.)
Downward: Surface with clear pattern and adequate lighting
(lux > 15)Detects diffuse reflective surfaces (>20%)
(walls, trees, people, etc.)

Remote Controller

Operating Frequency2.400 - 2.483 GHz;
5.725 - 5.850 GHz
Max Transmission Distance (unobstructed, free of interference)2.400 - 2.483 GHz; 5.725 - 5.850 GHz
FCC: 10000m
CE: 6000m
SRRC: 6000m
MIC: 6000m
Transmission Power (EIRP)2.400-2.4835 GHz:
25.5 dBm（FCC) ；18.5 dBm（CE) 19 dBm（SRRC) ；18.5 dBm（MIC)
5.725-5.850 GHz:
25.5 dBm（FCC) ；12.5 dBm（CE) 18.5 dBm（SRRC)
StorageROM 16GB + microSD Extensible Storage
Video Output PortHDMI Port
Built-in batteryType: 18650 Li-Po （5000 mAh @ 7.2 V)
Charging Mode: Charged with USB charger at 12V/2A
Rated Power 15 W
Charging time: 2 hr (with a USB charger at 12V/2A)
Operating Current/Voltage1800mA ⎓ 3.83V
Battery LifeBuilt-in Battery Approx. 2.5 hr
Operating Temperature-20 Deg. C - 40 Deg. C
RC SizeFolded without Joystick: 177.5 x 121.3 x 40 mm
Unfolded with Joystick: 177.5 x 181 x 60 mm
WeightApprox. 630 g
Intelligent Flight BatteryMain Link: 17.6V ⎓ 3.41A or 17.0V⎓3.53A
USB: 5.0 V ⎓ 2.0 A

Intelligent Flight Battery

Capacity[1]3850 mAh
Voltage15.4V
Max Charging Voltage17.6V
Battery TypeLiPo
Energy59.29 Wh
Net Weight297g
Charging Temperature5 Deg.C - 40 Deg.C
Operating Temperature Range-10 Deg.C - 40 Deg.C
Heating MethodsManual Heating, Auto Heating
Heating Temperature-20 Deg.C - 6 Deg.C
Heating duration500s (Max)
Heating Power55W (Max)
Charging Time90 mins
Max Charging Power80W

RTK Module

Dimensions69 mm x 69 mm x 59mm
ConnectionsMicro USB Port
RTK Positioning PrecisionIn RTK FIX
1cm+1ppm (Horizontal)
1.5cm+1 ppm (Vertical)

M2EA Spotlight

Dimensions68 x 60 x 41mm
ConnectionsMicro USB Port
Operating Range30 m
PowerMax 26W
IlluminanceFOV17 Deg., Max: 11lux @ 30m Straight

M2EA Beacon

Dimensions68mm x 40mm x 27.8mm
ConnectionsMicro USB Port
PowerAvg. 1.6W
Controllable Range5000 m
Light intensityMin Angle: 55 cd;
Light intensity: 157cd

M2EA Speaker

Dimensions68 x 55 x 65 mm
ConnectionsMicro USB Port
PowerMax 10W
Decibel100 db @ 1 meter distance
Max Bitrate16kbps

SD Cards

Supported SD CardsMicro SD™
Supports a microSD with capacity of up to 128 GB.
A UHS-I Speed Grade 3 rating microSD card is required.

App / Live View

Video Transmission SystemOcuSync 2.0
Mobile AppDJI PILOT(Android Version)
Live View QualityRemote Controller:
720p@30fps / 1080p@30fps
Max Live View Bitrate40Mbps
Latency120 - 130 ms
Required Operating Systemios 10.0 or later Android 5.0 or later

Others

Footnotes[1] The accuracy of the temperature measurement is measured at a distance of 5m against a blackbody with an emissivity of 0.95 under ideal conditions. The actual accuracy is also affected by various environmental factors such as temperature and humidity, and needs to be corrected by post-processing software. Under ideal conditions, the temperature accuracy can reach ±2 Deg.C or ±2%, whichever is greater.

[2] Omnidirectional Obstacle Sensing includes left/right, up/down, and forward/backward obstacle sensing. Sensing for left/right directions is only available in Tripod Mode. Omnidirectional Obstacle Sensing does not fully cover the circumference of a 360-degree arc. And left and right obstacle sensing system only works in specific modes and environments. DJI warranty does not cover any loss caused by crashing when flying left or right, even when Tripod mode is activated. Please be aware of your surroundings and App notifications when operating the Mavic 2 to ensure safety.
The terms HDMI, HDMI High-Definition Multimedia Interface, HDMI Trade dress and the HDMI Logos are trademarks or registered trademarks of HDMI Licensing Administrator, Inc.

Data source: https://www.dji.com/mavic-2-enterprise-advanced/specs

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Source data acquired 2023-01-23 19:03:43