Parameter

4.1 active aircraft control

Active aircraft control systems utilize sensors, fast controllers, and dynamic aerodynamic surfaces to actively manage flight stability and load distribution in real time. These technologies are critical for enabling lighter, ultra-high aspect ratio wing designs that drastically reduce aerodynamic drag. Challenges in developing these systems lie in creating ultra-fast, redundant control loops and actuators that comply with safety-critical aerospace airworthiness standards.

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
2
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