Parameter

4.1.8 active load alleviation

Active load alleviation systems utilize predictive sensors and automated control loops to rapidly adjust flight surfaces, mitigating structural stress caused by wind gusts and maneuvers. By damping peak bending moments, these systems allow engineers to design lighter, higher aspect ratio wings, saving significant airframe mass. Challenges in developing these systems lie in integrating ultra-fast LiDAR sensors and certifying safety-critical control software.

Hierarchy

4 technological themes
4.1 active aircraft control
4.1.1 variable camber
4.1.2 krueger flap
4.1.3 blown flap
4.1.4 novel high-lift devices
4.1.5 active canards
4.1.6 airflow control (active)
4.1.7 adaptive wing
4.1.8 active load alleviation
4.1.9 variable cg management
4.1.10 full autonomous flight control
4.1.11 fast control loops for load control
4.1.12 active nacelle
4.1.13 variable geometry nacelle
4.1.14 fast actuation for gust load alleviation
4.1.15 optimized fuel control
4.2 data transfer technologies
4.3 energy carriers
4.4 net zero technologies
4.5 operational technologies
4.6 aircraft propulsion
4.7 aircraft structures

Scenario relevance

Number of parameter occurrence per scenario.

Input
Output
1
2
Optimising together
N/A
Stripping down
N/A
Tech for you
N/A
Mad max

Milestone Timehorizon

PESTEL categories

Current

Short term

Medium term

Long term

Little to many relations with other Milestones