FEATURES
• Aggregation, computation, and soft noise filtering of data
from magnetometer, accelerometer, gyroscope, and other
integrated sensors
• Estimation of attitude stability to maintain consistent
posture during operation
• Algorithmic processing of speed, altitude, and flight-related
parameters according to programmed logic
• Integrated Kalman prediction filtering for state estimation
and trajectory maintenance based on INS guidance
combined with satellite signals
• PID-based computation of PWM values with real-time
adjustable parameters
• Data communication with the communication system,
supporting manual, semi-automatic, automatic, and
waypoint operating modes
• Autonomous operation capability with return-to-home and
INS-based navigation when satellite signals or data links are
unavailable
TECHNICAL SPECIFICATIONS
Software architecture includes sensor-data aggregation, waypoint and navigation modules, and computational/
analytical functions
EKF-3 algorithm for multi-source data fusion and accurate state estimation
Transmission-link noise filtering with corrupted-packet removal and error-notification capability
Safety fallback logic for loss of satellite signal, communication link, or low-power conditions
