DocumentCode :
583406
Title :
A hybrid differentiator for strapdown guidance system
Author :
Fan Jun-fang ; Su Zhong ; Li Qing ; Wang Jiang
Author_Institution :
Inst. of Intell. Control, Beijing Inf. Sci. & Technol. Univ., Beijing, China
fYear :
2012
fDate :
17-21 Oct. 2012
Firstpage :
1960
Lastpage :
1964
Abstract :
A strapdown guidance system for low-cost precise guided munitions is presented using strapdown small field-of-view (FOV) seeker and miniature inertial measurement unit (MIMU). The three-dimension line-of-sight (LOS) dynamics are described using the missile-target geometric transformation. Due to the weakness of strapdown seeker, a hybrid differentiator is then introduced to obtain and filter the inertial LOS rate for proportional guidance law. The analysis and trajectory simulation results verify the performance of the proposed algorithm.
Keywords :
missile guidance; missiles; hybrid differentiator; low-cost precise guided munitions; miniature inertial measurement unit; missile-target geometric transformation; strapdown guidance system; strapdown small field-of-view seeker; three-dimension line-of-sight dynamics; Detectors; Filtering algorithms; Gravity; Missiles; Trajectory; Hybrid differentiator; Proportional guidance law; Strapdown guidance;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Control, Automation and Systems (ICCAS), 2012 12th International Conference on
Conference_Location :
JeJu Island
Print_ISBN :
978-1-4673-2247-8
Type :
conf
Filename :
6393171
Link To Document :
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