ARIELOGIKAUTONOMOUS SYSTEMS // AL-Logic 1
SYS.06 // CLOSED-LOOP FLIGHT DYNAMICSISLAMABAD, PAKISTAN
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Real-time GNC

Engineered around control theory

Because inertial sensing, GNSS and telemetry live on the same board, AL-Logic 1 runs tight closed-loop guidance without companion-computer latency.

Reserve AL-Logic 1View specifications
24-STATE EKF3Attitude + positionL1 / TECSOuter guidanceCASCADED PID8 kHz + notch filterACTUATORS8 motor + 4 servoSENSOR FEEDBACK // IMU + GNSS ON THE SAME BOARD
Closed-loop flight dynamics, no companion computer in the loop
ESTIMATION

24-state EKF3

Attitude and position estimation feeding outer guidance.

INNER LOOP

Cascaded PID + notch

8 kHz gyro sampling with dynamic harmonic notch filtering to reject frame resonance.

FIXED-WING

L1 & TECS

Total Energy Control System couples pitch and throttle for airspeed and altitude tracking.

VTOL

Gain-scheduled transition

Automated hover-to-cruise blending with stall-margin protection.

SAFETY

Deterministic failsafe

Autonomous return-to-launch and loiter descent.

See the hardware on the AL-Logic 1 page.

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