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 :
بازگشت