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
Link To Document :
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