Engineering
Control Model
100%
Flight Control
100%
Rotors
100%
Aerodynamic Model
100%
Fault Tolerant Control
87%
Drone
50%
Aerodynamic Effect
50%
Failure (Mechanical)
50%
Accident Prevention
37%
Simplest Type
12%
Attitude Control
12%
High Energy Efficiency
12%
Drives
12%
Drone Delivery
12%
Development
12%
Major Part
12%
Model Uncertainty
12%
Rotor Pitch
12%
Unmanned Aerial Vehicle
12%
INIS
control
100%
aerodynamics
100%
rotors
75%
drone
41%
failures
33%
speed
25%
safety
25%
applications
16%
pitches
16%
algorithms
16%
energy efficiency
8%
attitude control
8%
torque
8%
attitudes
8%
lifts
8%
losses
8%
delivery
8%
disturbances
8%
performance
8%
unmanned aerial vehicles
8%