DocumentCode
3365933
Title
Study of algorithm for the ship´s instantaneous linear movement information based on SINS
Author
Jian-hua, Cheng ; Jun-yu, Shi ; Li-Cheng, Luo ; Jian-ming, Dong
Author_Institution
Sch. of Autom. Harbin Eng., Univ. Harbin, Harbin, China
fYear
2009
fDate
9-12 Aug. 2009
Firstpage
3364
Lastpage
3368
Abstract
Based on the important problem of the safe flying-off and landing of the warship-based aircrafts, this paper deeply analyze the ship´s linear movement characteristic and its calculation algorithm which can be realized by SINS. Firstly, the instantaneous linear movement is described by involving a new standard coordinate system. Then the linear movement information calculation algorithm based on SINS is given. By designing suitable high pass filter, the ships high frequency linear movement is properly extracted from the whole linear information. At last, the algorithm is certified by computer simulation and experimentation. Simulation and experimentation results show that this method can extract the high frequency linear movement information properly.
Keywords
aircraft landing guidance; inertial navigation; ships; SINS; high frequency linear movement information; high pass filter; ship instantaneous linear movement information; standard coordinate system; warship-based aircrafts flying-off; warship-based aircrafts landing; Aircraft; Algorithm design and analysis; Computer simulation; Data mining; Frequency; Information filtering; Information filters; Marine vehicles; Nonlinear filters; Silicon compounds; Digital high pass filter; Instantaneous movement; SINS; Warship-based aircraft;
fLanguage
English
Publisher
ieee
Conference_Titel
Mechatronics and Automation, 2009. ICMA 2009. International Conference on
Conference_Location
Changchun
Print_ISBN
978-1-4244-2692-8
Electronic_ISBN
978-1-4244-2693-5
Type
conf
DOI
10.1109/ICMA.2009.5246341
Filename
5246341
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