The system shall carry a payload of up to 2.5 kg.
System requirements
|
IS TESTED BY |
Payload capacity bench test: load 2.5 kg and verify stable h…
Qualification campaign
|
|
The system shall determine its position with an accuracy bet…
System requirements
|
IS TESTED BY |
Navigation accuracy test against surveyed ground truth.
Qualification campaign
|
|
The system shall detect obstacles larger than 5 cm at a rang…
System requirements
|
IS TESTED BY |
Obstacle detection bench test with a 5 cm wire target at 30 …
Qualification campaign
|
|
The system shall provide at least 35 minutes of flight endur…
System requirements
|
IS TESTED BY |
Endurance test: continuous hover until low-battery cutoff.
Qualification campaign
|
|
The system shall maintain a command-and-control link with le…
System requirements
|
IS TESTED BY |
C2 link range test at 8 km line-of-sight.
Qualification campaign
|
|
The system shall not exceed an acoustic level of 65 dB(A) at…
System requirements
|
IS TESTED BY |
Acoustic measurement at 50 m during simulated cruise.
Qualification campaign
|
|
The system shall deliver a parcel to any destination within …
System requirements
|
IS TESTED BY |
End-to-end range delivery flight to a destination 8 km away.
Flight test campaign
|
|
The system shall cruise at a nominal ground speed of 60 km/h…
System requirements
|
IS TESTED BY |
Cruise speed flight test on a 2 km straight leg.
Flight test campaign
|
|
The system shall complete a nominal delivery mission without…
System requirements
|
IS TESTED BY |
Fully autonomous mission from order to delivery, no operator…
Flight test campaign
|
|
The system shall not penetrate geofenced no-fly zones.
Safety & regulatory requirements
|
IS TESTED BY |
Geofence enforcement test: command a path crossing a no-fly …
Qualification campaign
|
|
When the battery state of charge drops below 15%, the system…
Safety & regulatory requirements
|
IS TESTED BY |
Low-battery safe landing test.
Qualification campaign
|
|
The system shall continuously broadcast a Remote ID signal a…
Safety & regulatory requirements
|
IS TESTED BY |
Remote ID broadcast verification with a regulatory receiver.
Qualification campaign
|
|
The system shall not exceed 120 m above ground level.
Safety & regulatory requirements
|
IS TESTED BY |
Maximum altitude limit test: command a climb above 120 m.
Qualification campaign
|
|
On loss of the C2 link for more than 10 s, the system shall …
Safety & regulatory requirements
|
IS TESTED BY |
Lost-link return-to-home test: C2 link cut in flight.
Flight test campaign
|
|
On detection of a critical failure, the system shall deploy …
Safety & regulatory requirements
|
IS TESTED BY |
In-flight parachute deployment test on commanded critical fa…
Flight test campaign
|
|
Manage mission
System functions
|
JUSTIFIES |
The system shall deliver a parcel to any destination within …
System requirements
|
|
Manage mission
System functions
|
JUSTIFIES |
The system shall complete a nominal delivery mission without…
System requirements
|
|
Manage payload
System functions
|
JUSTIFIES |
The system shall carry a payload of up to 2.5 kg.
System requirements
|
|
Navigate
System functions
|
JUSTIFIES |
The system shall determine its position with an accuracy bet…
System requirements
|
|
Detect & avoid obstacles
System functions
|
JUSTIFIES |
The system shall detect obstacles larger than 5 cm at a rang…
System requirements
|
|
Communicate (C2 & telemetry)
System functions
|
JUSTIFIES |
The system shall maintain a command-and-control link with le…
System requirements
|
|
Manage power
System functions
|
JUSTIFIES |
The system shall provide at least 35 minutes of flight endur…
System requirements
|
|
Ensure safety
System functions
|
JUSTIFIES |
The system shall not penetrate geofenced no-fly zones.
Safety & regulatory requirements
|
|
Ensure safety
System functions
|
JUSTIFIES |
On loss of the C2 link for more than 10 s, the system shall …
Safety & regulatory requirements
|
|
Manage power
System functions
|
JUSTIFIES |
When the battery state of charge drops below 15%, the system…
Safety & regulatory requirements
|
|
Ensure safety
System functions
|
JUSTIFIES |
On detection of a critical failure, the system shall deploy …
Safety & regulatory requirements
|
|
Autonomous navigation
System functions
|
REALIZES |
Deliver parcels autonomously across the city
Operational analysis
|
|
Reliable parcel delivery
System functions
|
REALIZES |
Deliver parcels autonomously across the city
Operational analysis
|
|
Detect & avoid air traffic
System functions
|
REALIZES |
Keep urban airspace safe
Operational analysis
|
|
Manage mission
System functions
|
REALIZES |
Supervise fleet & missions
Operational analysis
|
|
Manage mission
System functions
|
REALIZES |
Place delivery order
Operational analysis
|
|
Manage payload
System functions
|
REALIZES |
Receive parcel
Operational analysis
|
|
Ensure safety
System functions
|
REALIZES |
Authorize airspace use
Operational analysis
|
|
Autonomous urban parcel delivery
System functions
|
IS RELATED TO |
Autonomous navigation
System functions
|
|
Autonomous urban parcel delivery
System functions
|
IS RELATED TO |
Detect & avoid air traffic
System functions
|
|
Autonomous urban parcel delivery
System functions
|
IS RELATED TO |
Reliable parcel delivery
System functions
|
|
Autonomous navigation
System functions
|
IS RELATED TO |
Navigate
System functions
|
|
Detect & avoid air traffic
System functions
|
IS RELATED TO |
Detect & avoid obstacles
System functions
|
|
Reliable parcel delivery
System functions
|
IS RELATED TO |
Manage payload
System functions
|
|
Mission manager
Logical architecture
|
REALIZES |
Manage mission
System functions
|
|
Safety monitor
Logical architecture
|
REALIZES |
Ensure safety
System functions
|
|
State estimator
Logical architecture
|
REALIZES |
Navigate
System functions
|
|
Path planner
Logical architecture
|
REALIZES |
Navigate
System functions
|
|
Obstacle detector
Logical architecture
|
REALIZES |
Detect & avoid obstacles
System functions
|
|
Attitude controller
Logical architecture
|
REALIZES |
Stabilize & control flight
System functions
|
|
C2 link manager
Logical architecture
|
REALIZES |
Communicate (C2 & telemetry)
System functions
|
|
Power manager
Logical architecture
|
REALIZES |
Manage power
System functions
|
|
Payload controller
Logical architecture
|
REALIZES |
Manage payload
System functions
|
|
Flight computer board (NPU)
Physical architecture
|
REALIZES |
Flight Management Computer
Logical architecture
|
|
GNSS-RTK receiver
Physical architecture
|
REALIZES |
Navigation Subsystem
Logical architecture
|
|
LiDAR + stereo cameras
Physical architecture
|
REALIZES |
Sensing Subsystem
Logical architecture
|
|
4G/5G + RF C2 modem
Physical architecture
|
REALIZES |
Communication Subsystem
Logical architecture
|
|
Li-ion battery pack (6S)
Physical architecture
|
REALIZES |
Power Subsystem
Logical architecture
|
|
4× BLDC motors + ESC
Physical architecture
|
REALIZES |
Flight Control Subsystem
Logical architecture
|
|
Emergency parachute module
Physical architecture
|
REALIZES |
Flight Management Computer
Logical architecture
|
|
Standby (on ground)
Flight modes & states
|
IS RELATED TO |
Manage mission
System functions
|
|
Takeoff
Flight modes & states
|
IS RELATED TO |
Stabilize & control flight
System functions
|
|
Cruise
Flight modes & states
|
REALIZES |
The system shall cruise at a nominal ground speed of 60 km/h…
System requirements
|
|
Cruise
Flight modes & states
|
REALIZES |
The system shall not exceed an acoustic level of 65 dB(A) at…
System requirements
|
|
Cruise
Flight modes & states
|
IS RELATED TO |
Navigate
System functions
|
|
Delivery hover
Flight modes & states
|
REALIZES |
The system shall deliver a parcel to any destination within …
System requirements
|
|
Delivery hover
Flight modes & states
|
REALIZES |
The system shall complete a nominal delivery mission without…
System requirements
|
|
Delivery hover
Flight modes & states
|
IS RELATED TO |
Manage payload
System functions
|
|
Return to home
Flight modes & states
|
REALIZES |
On loss of the C2 link for more than 10 s, the system shall …
Safety & regulatory requirements
|
|
Return to home
Flight modes & states
|
IS RELATED TO |
Ensure safety
System functions
|
|
Landing
Flight modes & states
|
REALIZES |
When the battery state of charge drops below 15%, the system…
Safety & regulatory requirements
|
|
Emergency recovery
Flight modes & states
|
REALIZES |
On detection of a critical failure, the system shall deploy …
Safety & regulatory requirements
|
|
Emergency recovery
Flight modes & states
|
IS RELATED TO |
Ensure safety
System functions
|
|
Charging (on ground)
Battery management states
|
IS RELATED TO |
Manage power
System functions
|
|
Healthy (SoC > 40%)
Battery management states
|
REALIZES |
The system shall provide at least 35 minutes of flight endur…
System requirements
|
|
Healthy (SoC > 40%)
Battery management states
|
IS RELATED TO |
Manage power
System functions
|
|
Critical (< 15%)
Battery management states
|
REALIZES |
When the battery state of charge drops below 15%, the system…
Safety & regulatory requirements
|
|
Critical (< 15%)
Battery management states
|
IS RELATED TO |
Ensure safety
System functions
|
|
GNSS position drift beyond 0.5 m under urban multipath
Technical issues
|
IS RELATED TO |
The system shall determine its position with an accuracy bet…
System requirements
|
|
GNSS position drift beyond 0.5 m under urban multipath
Technical issues
|
IS RELATED TO |
Navigate
System functions
|
|
GNSS position drift beyond 0.5 m under urban multipath
Technical issues
|
IS RELATED TO |
Navigation accuracy test against surveyed ground truth.
Qualification campaign
|
|
Flight endurance short of 35 min at full payload in cold wea…
Technical issues
|
IS RELATED TO |
The system shall provide at least 35 minutes of flight endur…
System requirements
|
|
Flight endurance short of 35 min at full payload in cold wea…
Technical issues
|
IS RELATED TO |
The system shall carry a payload of up to 2.5 kg.
System requirements
|
|
Flight endurance short of 35 min at full payload in cold wea…
Technical issues
|
IS RELATED TO |
Manage power
System functions
|
|
Flight endurance short of 35 min at full payload in cold wea…
Technical issues
|
IS RELATED TO |
Endurance test: continuous hover until low-battery cutoff.
Qualification campaign
|
|
Obstacle detection misses thin wires near the 5 cm / 30 m li…
Technical issues
|
IS RELATED TO |
The system shall detect obstacles larger than 5 cm at a rang…
System requirements
|
|
Obstacle detection misses thin wires near the 5 cm / 30 m li…
Technical issues
|
IS RELATED TO |
Detect & avoid obstacles
System functions
|
|
Obstacle detection misses thin wires near the 5 cm / 30 m li…
Technical issues
|
IS RELATED TO |
Obstacle detection bench test with a 5 cm wire target at 30 …
Qualification campaign
|
|
C2 link packet loss exceeds 2% beyond 7 km
Technical issues
|
IS RELATED TO |
The system shall maintain a command-and-control link with le…
System requirements
|
|
C2 link packet loss exceeds 2% beyond 7 km
Technical issues
|
IS RELATED TO |
Communicate (C2 & telemetry)
System functions
|
|
C2 link packet loss exceeds 2% beyond 7 km
Technical issues
|
IS RELATED TO |
C2 link range test at 8 km line-of-sight.
Qualification campaign
|
|
Acoustic level exceeds 65 dB(A) during aggressive climb
Technical issues
|
IS RELATED TO |
The system shall not exceed an acoustic level of 65 dB(A) at…
System requirements
|
|
Acoustic level exceeds 65 dB(A) during aggressive climb
Technical issues
|
IS RELATED TO |
Acoustic measurement at 50 m during simulated cruise.
Qualification campaign
|
|
Return-to-home triggered late after simulated C2 loss
Technical issues
|
IS RELATED TO |
On loss of the C2 link for more than 10 s, the system shall …
Safety & regulatory requirements
|
|
Return-to-home triggered late after simulated C2 loss
Technical issues
|
IS RELATED TO |
Ensure safety
System functions
|
|
Return-to-home triggered late after simulated C2 loss
Technical issues
|
IS RELATED TO |
Lost-link return-to-home test: C2 link cut in flight.
Flight test campaign
|
|
Parachute deployment delayed on critical failure injection
Technical issues
|
IS RELATED TO |
On detection of a critical failure, the system shall deploy …
Safety & regulatory requirements
|
|
Parachute deployment delayed on critical failure injection
Technical issues
|
IS RELATED TO |
Ensure safety
System functions
|
|
Parachute deployment delayed on critical failure injection
Technical issues
|
IS RELATED TO |
In-flight parachute deployment test on commanded critical fa…
Flight test campaign
|
|
Geofence buffer too small near no-fly boundary
Technical issues
|
IS RELATED TO |
The system shall not penetrate geofenced no-fly zones.
Safety & regulatory requirements
|
|
Geofence buffer too small near no-fly boundary
Technical issues
|
IS RELATED TO |
Navigate
System functions
|
|
Geofence buffer too small near no-fly boundary
Technical issues
|
IS RELATED TO |
Geofence enforcement test: command a path crossing a no-fly …
Qualification campaign
|
|
C2 radio link (drone ↔ ground station)
Interfaces
|
CONNECTS |
Communicate (C2 & telemetry)
System functions
|
|
C2 radio link (drone ↔ ground station)
Interfaces
|
CONNECTS |
Ground control station
System functions
|
|
C2 radio link (drone ↔ ground station)
Interfaces
|
IS RELATED TO |
The system shall maintain a command-and-control link with le…
System requirements
|
|
C2 radio link (drone ↔ ground station)
Interfaces
|
IS TESTED BY |
C2 link range test at 8 km line-of-sight.
Qualification campaign
|
|
GNSS-RTK correction feed
Interfaces
|
CONNECTS |
Navigate
System functions
|
|
GNSS-RTK correction feed
Interfaces
|
IS RELATED TO |
The system shall determine its position with an accuracy bet…
System requirements
|
|
GNSS-RTK correction feed
Interfaces
|
IS TESTED BY |
Navigation accuracy test against surveyed ground truth.
Qualification campaign
|
|
Payload bay mechanical & power interface
Interfaces
|
CONNECTS |
Manage payload
System functions
|
|
Payload bay mechanical & power interface
Interfaces
|
IS RELATED TO |
The system shall carry a payload of up to 2.5 kg.
System requirements
|
|
Payload bay mechanical & power interface
Interfaces
|
IS TESTED BY |
Payload capacity bench test: load 2.5 kg and verify stable h…
Qualification campaign
|
|
Main power bus
Interfaces
|
CONNECTS |
Manage power
System functions
|
|
Main power bus
Interfaces
|
IS RELATED TO |
The system shall provide at least 35 minutes of flight endur…
System requirements
|
|
Perception sensor data bus
Interfaces
|
CONNECTS |
Detect & avoid obstacles
System functions
|
|
Perception sensor data bus
Interfaces
|
IS RELATED TO |
The system shall detect obstacles larger than 5 cm at a rang…
System requirements
|
|
Perception sensor data bus
Interfaces
|
IS TESTED BY |
Obstacle detection bench test with a 5 cm wire target at 30 …
Qualification campaign
|
|
Customer delivery notifications API
Interfaces
|
CONNECTS |
Customer mobile app
System functions
|
|
Customer delivery notifications API
Interfaces
|
IS RELATED TO |
The system shall complete a nominal delivery mission without…
System requirements
|
|