DocumentCode
3407798
Title
High Accuracy Acquisition of the Magnetic Heading Signal
Author
Duan, Fengyang ; Sun, Baixiang ; Zhang, Lijing
Author_Institution
Air Force Aviation Univ., Changchun
fYear
2007
fDate
5-8 Aug. 2007
Firstpage
2304
Lastpage
2308
Abstract
The function of the fluxgate sensor in the aircraft navigation system is to calibrate the heading of gyro. Its magnetic heading signal is weak and anomalous synchro signal. Experimental results show that this signal cannot be measured directly and exactly by using SDC. This paper designs a negative feedback amplifying circuit which uses the servo amplifying setup and synchronizer equipment to convert the magnetic heading signal to the standard synchro signal. Meanwhile, we study and manufacture the SDC and DSC modules which integrate the multifunction based-on PC-104 bus synchro/digital converting card. In the practical operation, we adopt the above-mentioned scheme and calibrate the compass error by the software. The result demonstrates that the acquisition accuracy of magnetic heading signal reaches 0.1deg and meets the demands of the navigation accuracy.
Keywords
aircraft navigation; amplifiers; feedback; servomechanisms; signal detection; PC-104 bus synchro-digital converting card; aircraft navigation system; fluxgate sensor function; magnetic heading signal acquisition; navigation accuracy; negative feedback amplifying circuit; servo amplifying setup; synchronizer equipment; Aircraft navigation; Feedback circuits; Integrated circuit measurements; Magnetic circuits; Magnetic devices; Magnetic sensors; Negative feedback; Sensor systems; Servomechanisms; Signal design; Digital converting; Magnetic heading measurement; Servo amplifier; synchronizer;
fLanguage
English
Publisher
ieee
Conference_Titel
Mechatronics and Automation, 2007. ICMA 2007. International Conference on
Conference_Location
Harbin
Print_ISBN
978-1-4244-0828-3
Electronic_ISBN
978-1-4244-0828-3
Type
conf
DOI
10.1109/ICMA.2007.4303912
Filename
4303912
Link To Document