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LOS stabilization of optic-electro landing system
Ge B.; Gao H.-B.; Yu Y.
2014
发表期刊Guangxue Jingmi Gongcheng/Optics and Precision Engineering
ISSNISBN/1004924X
卷号22期号:6页码:1577-1583
摘要To increase line-of-sight (LOS) tracking and pointing accuracy of an Optic-Electro (O-E) landing guidance system, this work explores how to isolate the LOS tracking and pointing of a O-E theodolite from the carrier motion disturbance. A carrier-based O-E theodolite model was established with various disturbance factors introduced. Three kinds of controllers, Lead-lag, LQG/LTR(Linear Quadratic Gaussian/Loop Transfer Recovery) and H were designed to improve the stability and performance of the system. The Kalman filter and H weighting matrix were investigated in detail. Then, the controllers were emulated in Matlab and verified on a swing bench. The compared experiments for the three kinds of controllers on time domain, frequency response and stability were performed. Obtained results show that both LQG/LTR and H controllers can satisfy the design specifications, and their decoupling effects are as deep as 50 dB, which can ensure precise tracking and pointing performance of LOSs in O-E landing guidance systems.
收录类别EI
语种中文
文献类型期刊论文
条目标识符http://ir.ciomp.ac.cn/handle/181722/44133
专题中科院长春光机所知识产出
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GB/T 7714
Ge B.,Gao H.-B.,Yu Y.. LOS stabilization of optic-electro landing system[J]. Guangxue Jingmi Gongcheng/Optics and Precision Engineering,2014,22(6):1577-1583.
APA Ge B.,Gao H.-B.,&Yu Y..(2014).LOS stabilization of optic-electro landing system.Guangxue Jingmi Gongcheng/Optics and Precision Engineering,22(6),1577-1583.
MLA Ge B.,et al."LOS stabilization of optic-electro landing system".Guangxue Jingmi Gongcheng/Optics and Precision Engineering 22.6(2014):1577-1583.
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