Skip to main navigation
Skip to search
Skip to main content
Beijing Institute of Technology Home
English
中文
Home
Profiles
Research units
Research output
Prizes
Search by expertise, name or affiliation
View Scopus Profile
Li Mo
School of Aerospace Engineering
h-index
49
Citations
3
h-index
Calculated based on number of publications stored in Pure and citations from Scopus
2009
2024
Research activity per year
Overview
Fingerprint
Network
Research output
(15)
Similar Profiles
(2)
Fingerprint
Dive into the research topics where Li Mo is active. These topic labels come from the works of this person. Together they form a unique fingerprint.
Sort by
Weight
Alphabetically
Engineering
Actuator Disk
20%
Actuator Failure
6%
Aerodynamic Interference
40%
Aerodynamics
20%
Air Superiority
10%
Aircraft Aerodynamics
6%
Airframe-Propulsion Integration
6%
Attitude Control
20%
Brushless Motor
6%
Computational Domain
6%
Computational Fluid Dynamics
18%
Computer Simulation
6%
Control System
6%
Conversion Process
13%
Decision Parameter
20%
Design Method
20%
Dynamic Method
8%
Electric Propulsion
20%
Experimental Result
9%
External Disturbance
6%
Feedback Control System
6%
Fixed Pitch Propeller
6%
Fixed Wings
20%
Flight Trajectory
17%
Flow Field
6%
Forward Speed
6%
Fourier Series
20%
Mechanical Power
20%
Model Geometry
6%
Non-Linear Dynamic
20%
Numerical Study
20%
Objective Function
6%
Obstacle Avoidance
20%
Obtains
8%
Pitching Moment
7%
Power Conversion
13%
Power Input
13%
Propulsion System
20%
Radial Basis Function
6%
Reinforcement Learning
30%
Rotors
40%
Sampling Error
6%
Simulation Result
20%
Singularities
6%
Space Solution
20%
State Variable
20%
System State
20%
Transients
26%
Transport Aircraft
20%
Unmanned Aerial Vehicle
100%
Computer Science
actuator fault
6%
Control Approach
6%
Control Framework
6%
Decision Method
6%
Decision-Making
29%
Fault Tolerant
20%
Information Synthesis
5%
Inherent Complexity
6%
Interpretability
6%
Managing System
6%
multiple robot
20%
Nonlinear Interaction
6%
Numerical Simulation
6%
Obstacle Avoidance
20%
radial base function neural network
6%
Robot
20%
Sampling Error
6%
Solution Space
6%
State Variable
6%
Triggered Event
20%
Unmanned Aerial Vehicle
40%
Unmanned Aerial Vehicle
20%
