check_circle
Parameters updated
HARDWARE CONSOLE
CFG-MOD: ACTIVE
Device Settings & Radio Bus
LINK STATUS:
SYNCHRONIZED (100%)
EEPROM PARAMS:
1,142 / 1,142 LOADED
cell_tower
Telemetry & Radio Link Bus
RFD900X ONLINE
DEVICE TTY PORT
/dev/ttyUSB0
cable
Silicon Labs CP210x
HARDWARE TRANSCEIVER
RFD900x Ultra
915MHz
Dual Ant / Diversity OK
TRANSMISSION BAUDRATE
NET ID (FHSS MASK)
25
TX POWER OUTPUT
20 dBm (100mW)
check
RTS/CTS Hardware Flow Control
lock
MAVLink 2.0 Auth & Encryption
RF LINK ATTENUATION & DIVERSITY NOISE
RSSI: 94% (-68 dBm)
TX BUFFER: 0% DROPS
NOISE FLOOR: -102 dBm
REMOTE RSSI: 91%
cloud_sync
Cloud Sync & Survey Logs
BHARAT GEOCLOUD OK
GCS NVMe DRIVE
128 GB
USED: 53.7 GB (42%)
FREE: 74.3 GB
GEODETIC SURVEY PIPE
RINEX / GNSS
cloud_done
Raw Observation Auto-Sync
sync
Auto-upload Mission Flight Telemetry (.BIN / .TLOG)
ACTIVE
photo_library
Sony EXIF Geotag Metadata Extraction
READY
system_update_alt
ArduPilot 4.5.1 Firmware Check
UP TO DATE
tune
Vehicle Parameters & Failsafes
HEXACOPTER X-FRAME
X6 ENTERPRISE (6 ROTORS)
FRAME MOTOR GEOMETRY (HEXA-X 6-ROTOR CW/CCW)
AIRFRAME: READY TO ARM
FRONT (M1/M6)
MID (M2/M5)
REAR (M3/M4)
DGCA GEOFENCE BOUNDARIES (INDIA DIGITAL SKY COMPLIANT)
GREEN ZONE FLIGHT REGIME
MAX ALTITUDE (AGL)
120
METERS
DGCA HARD CEILING
MAX HORIZONTAL RADIUS
1,500
METERS
CADASTRE BUFFER OK
BREACH ACTION
RTL
@ 60m
AUTO RETURN TO HOME
CRITICAL FAILSAFE DIRECTIVES
RTL MODE
LAND NOW
RTL RETURN
CONTINUE
Low Battery RTL
Trigger at < 21.6V (6S LiPo 20%)
Critical Battery Cutoff
Trigger at < 20.4V (Emergency Land)
RC Signal Loss (>3.0s)
Telemetry receiver failsafe timeout
GCS Link Disconnect
Continue survey waypoint auto-path
view_in_ar
Pre-Flight Sensor Calibration
IMU SENSORS: DUAL ICM-42688P
6-Axis Accelerometer
CALIBRATED
Last calibration completed 2 days ago. Residual noise 0.04 m/s².
Dual Magnetometer
OFFSETS OK
OFFSETS:
X: -42
Y: +18
Z: +110
Horizon Level Zero
ROLL: 0.1° | PITCH: -0.2°
Ensure drone is on perfectly leveled ground before setting zero.
ESC / Motor Bench Test
PROPS OFF REQUIRED
Sequentially spins M1 → M2 → M3 → M4 at 10% throttle for spin direction verification.
list_alt
ArduPilot EEPROM Parameters Table
| PARAM NAME | VALUE | DESCRIPTION | GROUP |
|---|