DocumentCode :
1980806
Title :
LOS rate reconstruction and application of roll-pitch seeker
Author :
Yang, Chunlei ; Zhang, Nan ; Jia, Hongguang
Author_Institution :
New Technol. Dept., Changchun Inst. of Opt., Fine Mech. & Phys., Changchun, China
fYear :
2011
fDate :
16-18 Sept. 2011
Firstpage :
2307
Lastpage :
2310
Abstract :
Frame motion form of roll-pitch seeker is introduced in this paper. There is corresponding relationship between the frame angle of the roll-pitch seeker and the traditional yaw-pitch seeker. The discrepancy of line-of-sight (LOS) rate of the two seekers is caused by the different frame motion forms. LOS rate reconstruction method of roll-pitch seeker is deduced. Compared to the pure proportional navigation guidance law, the true proportional navigation guidance law is more suitable for the roll-pitch seeker missile guidance.
Keywords :
missile guidance; LOS rate reconstruction method; frame motion forms; missile guidance; proportional navigation guidance law; roll-pitch seeker; yaw-pitch seeker; Active appearance model; Laser modes; Navigation; Physics; Reconstruction algorithms; Zirconium; LOS rate; proportional guidance law; roll-pitch seeker; yaw-pitch seeker;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Electrical and Control Engineering (ICECE), 2011 International Conference on
Conference_Location :
Yichang
Print_ISBN :
978-1-4244-8162-0
Type :
conf
DOI :
10.1109/ICECENG.2011.6057415
Filename :
6057415
Link To Document :
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