The integrated flight controller is a high-precision navigation control unit designed to provide stable, reliable, and real-time flight control performance in complex and dynamic environments. This system integrates advanced inertial sensing, navigation algorithms, and control logic into a compact structure, ensuring accurate motion sensing and rapid response capabilities.
Optimized for platforms requiring high stability, rapid alignment, and precise navigation, this controller delivers consistent performance even under high-dynamic and vibration conditions.
Angular velocity range: -200°/s to +200°/s
Low zero-point deviation, high stability
Low proportional factor nonlinearity, low crosstalk
Measurement Range: -10g to +10g (maximum ±15g axial)
Low zero-point deviation, high stability
High bandwidth response in dynamic environments
Initial alignment attitude error ≤1.0°
Position accuracy within 120 meters (short-term solution)
Attitude accuracy within 1.6°
| Product Name | Integrated flight controller |
|---|---|
|
Accelerometer measurement range |
-10g~10g, (axial -15g~15g). |
|
Accelerometer zero bias |
≤ 15mg (3σ) |
|
Accelerometer zero bias stability |
≤ 15mg (3σ) |
|
Accelerometer scale factor non-linearity |
≤ 500ppm |
|
Accelerometer cross-coupling coefficient |
≤ 500ppm |
|
Accelerometer bandwidth: |
≥ 70Hz (phase lag 90° |
|
Navigation initial alignment attitude error |
≤1.0° (3σ) |
|
Initial alignment time |
≤ 40s |
|
Navigation solution position error within 18s |
≤120m (3σ) |
|
Navigation solution attitude error (including initial alignment error) within 18s |
≤ 1.6° (3σ) |
The integrated flight controller is suitable for systems requiring precise navigation and stable control performance
It provides real-time navigation, motion sensing, and flight control in a single integrated unit.
The initial alignment time is ≤40 seconds.
Yes, with high bandwidth sensors and stable performance, it is designed for dynamic conditions.
