Parameter

4.1.5 active canards

Active canards are small, dynamically controlled horizontal foreplanes mounted near the nose of an aircraft to actively manage pitch, trim, and structural load distribution in flight. By adjusting their angle of attack in real time, these surfaces can suppress gust loads and reduce trim drag, directly improving fuel efficiency. Challenges in developing these surfaces lie in managing their aeroelastic interaction with the main wing and ensuring fast, redundant control actuation.

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