🟢 SYSTEM STATUS: NOMINAL
🔥 IGNIS 🔥
THRUST VECTOR CONTROL SYSTEM // MISSION READY
▼ MISSION STATUS ▼
📡 LIVE TELEMETRY
Real-time sensor data from IGNIS-CORE flight computer
📡 ALTITUDE CONTROL ● LIVE
PITCH 2.4 °
ROLL -1.2 °
YAW 0.8 °
CONTROL MODE ACTIVE
📡 ENVIRONMENT ● LIVE
ALTITUDE 124.5 m AGL
PRESSURE 1013.2 hPa
TEMPERATURE 24.8 °C
VELOCITY 12.3 m/s
📡 GPS STATUS ● LIVE
LATITUDE 28.6139 °N
LONGITUDE 77.2090 °E
SAT FIX 8 sats
HDOP 1.2
📡 SYSTEM HEALTH ● LIVE
CPU LOAD 23 %
MEMORY 42 KB free
LOOP TIME 10 ms
UPTIME 03:24:17
🎯 SYSTEM OVERVIEW
Mission-critical components for active thrust vectoring
PRECISION CONTROL
Real-time altitude control with complementary filter and PID algorithm for stable flight.
LORA TELEMETRY
Long-range telemetry up to 5km with SX1278 module for real-time data monitoring.
GPS TRACKING
NEO-6M GPS module for position tracking, speed, and altitude data.
MODULAR DESIGN
Separate modules for sensor hub, TVC mechanism, and ground station.
🛸 3D INTERACTIVE MODEL
Explore the IGNIS rocket assembly in 3D space
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🖱️ DRAG TO ROTATE •
🔍 SCROLL TO ZOOM •
🎮 RIGHT-CLICK TO PAN
100+
HOURS OF DEVELOPMENT
3
MODULES
5KM
TELEMETRY RANGE
50HZ
CONTROL LOOP