DocumentCode :
3722648
Title :
Guidance Law Design Based on Finite Time Convergence
Author :
Yanli Yang;Lihua Chen;Zhiguo Liu;Guoliang Zhang
Author_Institution :
High-Tech Inst. of Xi´an, Xi´an, China
fYear :
2015
Firstpage :
240
Lastpage :
245
Abstract :
Traditional guidance laws are designed based on Lyapunov theorem. They will guide the line of sight (LOS) angular rate to converge to zero when time approaches infinity. In this paper, guidance laws with finite time convergence are proposed in terms of finite time stability theory of nonlinear control systems. It is proved that the LOS angular rate will converge to zero before the final guidance ends with the designed guidance laws. Simulation results show that the guidance laws are highly effective.
Keywords :
"Missiles","Acceleration","Convergence","Stability analysis","Mathematical model","Nonlinear systems","Electronic mail"
Publisher :
ieee
Conference_Titel :
Computer Science and Mechanical Automation (CSMA), 2015 International Conference on
Type :
conf
DOI :
10.1109/CSMA.2015.55
Filename :
7371659
Link To Document :
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