Overview
H11 ACROS SW-12 is a blended-wing flight demonstrator created to validate morphing surfaces, distributed structural sensing, efficient propulsion integration, and real-time aerodynamic optimization.
H11 Systems
Adaptive smart-wing flight demonstrator
H11 ACROS SW-12™
An aircraft that measures and reshapes its aerodynamic state in flight.
ACROS SW-12 develops the H11 Smart Wing System into a flyable research platform where distributed load sensing, compliant surfaces, and adaptive control work as one aero-structural loop.
Grounded in the H11 Smart Wing concept
Uses measurable bounded adaptation
Built as a realistic flight demonstrator
System Overview
H11 ACROS SW-12™ in context.
What It Does
It records wing load and airflow state during flight, commands small verified surface-shape changes, and measures their effect on stability, drag, control authority, and energy use.
How It Works
Embedded pressure and strain sensing feeds a bounded flight controller. Electromechanical morphing structures adjust camber and local twist within certified limits while conventional controls remain available.
Capabilities
Operational strengths built into the platform.
Each page below is derived from the whitepaper content in the workspace and reframed as a deployment-facing product profile for H11 Systems.
Distributed wing load sensing
Bounded adaptive camber control
Aero-structural flight-data capture
Efficient blended airframe research
Conventional control fallback
Adaptive flight architecture
Integrated with the rest of the H11 stack.
Morphing wing structures
Distributed aerodynamic sensing
ACROS adaptive control loop
Instrumented research-aircraft platform
Applications
Where this system fits.
Smart-wing flight research
Long-endurance survey aircraft
Efficient transport configuration studies
Aeroelastic control validation