Wind tunnel evaluation for control transition from elevator to stabilator of small UAV
Faulty control surface actuator in a small Unmanned Aerial Vehicles (sUAV) could be overcome with a few techniques. Redundant actuators, analytical redundancy or combination of both are normally used as fault accommodation techniques. In this paper, the accommodation technique of faulty elevator act...
Main Authors: | , , , |
---|---|
Format: | Article |
Language: | English |
Published: |
2018
|
Online Access: | http://dspace.uniten.edu.my/jspui/handle/123456789/6938 |