Old Web
English
Sign In
Acemap
>
Paper
>
A nonlinear guidance and active fault tolerant control system for a fixed wing Unmanned Aerial Vehicle
A nonlinear guidance and active fault tolerant control system for a fixed wing Unmanned Aerial Vehicle
2010
Bertoni
Bertozzi
Castaldi
Simani
Keywords:
Trajectory
Exponential stability
Feedback linearization
Nonlinear system
Control theory
Active fault
Adaptive filter
Remotely operated underwater vehicle
Control system
Computer science
Correction
Source
Cite
Save
Machine Reading By IdeaReader
0
References
0
Citations
NaN
KQI
[]