DocumentCode
1621440
Title
Delayed feedback altitude control for micro UAV without sensing pitch rate
Author
Kojima, Ryota ; Ogawara, Kakuji ; Yoneda, Takahiro ; Tomoigawa, Shinji
fYear
2008
Firstpage
316
Lastpage
319
Abstract
In this paper we demonstrate characteristics of DFC in the situation that pitch rate and A.O.A. are unknown. This paper demonstrates characteristics of delayed feedback control in the case of pitch rate sensor´s absence.
Keywords
aircraft; attitude control; delays; feedback; optical sensors; remotely operated vehicles; angle of attack; attitude stabilizing apparatus; delayed feedback altitude control; infrared thermo sensors; micro UAV; pitch angle; Airplanes; Automatic control; Control systems; Delay; Digital-to-frequency converters; Feedback; Global Positioning System; Sensor systems; Temperature sensors; Unmanned aerial vehicles;
fLanguage
English
Publisher
ieee
Conference_Titel
Control, Automation and Systems, 2008. ICCAS 2008. International Conference on
Conference_Location
Seoul
Print_ISBN
978-89-950038-9-3
Electronic_ISBN
978-89-93215-01-4
Type
conf
DOI
10.1109/ICCAS.2008.4694663
Filename
4694663
Link To Document