Parameter

4.1.11.1 cargo shift for optimal balance (electric flight)

Cargo shift for optimal balance (electric flight) is an automated system that physically repositions cargo during electric flight to maintain the ideal center of gravity. Unlike conventional aircraft that become lighter as fuel is burned, battery-electric aircraft maintain a constant mass, making dynamic balance management important. Challenges in developing this system include designing safe mechanical tracks and integrating precise weight-distribution sensors.

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
4.1.11.1 cargo shift for optimal balance (electric flight)
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