Euronext | ALUAV | € 32.00 | 09/15/2026

Helicopter UAVs require highly responsive flight control systems to manage dynamic rotorcraft aerodynamics. Veronte Autopilot offers certified-level stability, rotor coordination, and autonomous operation, enabling complex and high-precision missions from any platform size, including manned and unmanned operations.

Helicopter Layout Compatibility

Conventional Rotorcraft

Conventional Rotorcraft

Main rotor with tail rotor configuration.

Coaxial Helicopter

Coaxial Helicopter

Dual counter-rotating rotors with torque-neutral design.

Tandem Rotor

Tandem Rotor

Twin rotor systems providing enhanced lift and payload.

Intermeshing Rotor (Synchropter)

Intermeshing Rotor (Synchropter)

Intersecting rotors for compact, high-stability applications.

Takeoff and Landing Capabilities

Takeoff

Takeoff

Veronte enables vertical autonomous liftoff with precise control. Compatible with takeoff from ships, vehicles, or confined field locations. Algorithms ensure smooth climb under dynamic conditions.

Landing

Landing

Includes autonomous touchdown, precision relative landing, and energy-aware descent profiles. Vision-aided, GPS RTK and relative positioning sensor integration enable high-repeatability landing in varied conditions.

Flight Control for Helicopter

Full support for cyclic, collective, and tail rotor control with real-time feedback loops. Flight logic includes autorotation support for emergency glide-down and wind adaptation for high-resilience performance.

Mission Capabilities & Precision Operations

Ship-Based Operations

Coordinated landing and takeoff from moving vessels.

Search & Rescue

Hover, scan, and delivery capabilities with autonomous payload deployment.

Infrastructure Survey

Low-altitude inspection with camera stabilization.

Synchronize missions with other aerial assets.

Multi-Helicopter Coordination

Custom Mission Blocks

Triggered actions and logic-phase sequencing.

Redundancy, Safety and Compliance

Designed for critical safety, Veronte supports triple-redundant configurations, health telemetry, and customizable emergency behavior (e.g., autorotation, return-to-ship). Developed under DO-178C / DO-254 standards.

Advanced Features for Helicopter

Rotor Governor Mode

Maintain stable rotor RPM across load changes.

Autorotation Support

Dynamic autorotation entry and control.

Relative Landing on Moving Platforms

GPS and visual marker-based alignment.

Flexible Engine Control

Adaptable for turbine, piston, or hybrid-electric.