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BHOOMI DRISHTI GCS v2.4-RC3

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Profile
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
ACTIVE
lock
MAVLink 2.0 Auth & Encryption
SHA-256 SIGNED
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
M1 (CCW) M5 (CW) M3 (CCW) M4 (CW) M2 (CCW) M6 (CW)
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
Low Battery RTL
Trigger at < 21.6V (6S LiPo 20%)
RTL MODE
Critical Battery Cutoff
Trigger at < 20.4V (Emergency Land)
LAND NOW
RC Signal Loss (>3.0s)
Telemetry receiver failsafe timeout
RTL RETURN
GCS Link Disconnect
Continue survey waypoint auto-path
CONTINUE
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