Product overview
The Chongqing Tianjian Inertial Technology Co., Ltd. 8K22A integrated navigation system provides position, velocity and attitude information for UAVs and experimental rockets. Its internal architecture combines MEMS gyroscopes and accelerometers with a high-dynamic satellite navigation receiver, navigation computer, power conversion circuitry and interface circuitry. Integrated navigation or pure inertial navigation algorithms process the carrier’s measurements. Functions include self-test, self-alignment, transfer-alignment parameter loading, transfer alignment, online upgrades, simulation and information exchange. Stationary-base self-alignment takes ≤60s, while the satellite receiver operates on B1/L1 with a 10Hz data update rate.
The main unit weighs ≤300g, excluding supporting cables, the antenna and associated test cables, and measures ≤96mm×64mm×42mm. It accepts DC16V–36V, with steady-state current below 0.5A and steady-state power consumption ≤10W. Two RF inputs are combined. Integrated navigation delivers horizontal position accuracy of ≤10m RMS, elevation accuracy of ≤12m RMS and velocity accuracy of ≤0.2m/s at 1σ. Heading accuracy is ≤5° at 3σ, and attitude accuracy is ≤3° at 3σ. Operating temperature is -40°C to +60°C; storage temperature is -45°C to +70°C.
