DocumentCode :
3291907
Title :
A sliding-mode based guidance law for intercepting missile with passive ranging law
Author :
Po-Hsu Huang ; Ting-Kuo Wang ; Li-Chen Fu
Author_Institution :
Electr. Eng. Dept., Nat. Taiwan Univ., Taipei, Taiwan
fYear :
2010
fDate :
June 30 2010-July 2 2010
Firstpage :
2082
Lastpage :
2087
Abstract :
This paper proposes the development and implementation of the sliding-mode based guidance law with a passive 3-D ranging law by using angle-only measurements (e.g. IR image sensor data). The passive ranging law applies the Modified Spherical Coordinates (MSC) based method and the well-known Extended Kalman filter technique to conduct further analysis for the tracking. In addition, The Interacting Multiple Model (IMM) technique coupled with multiple sub-filters of ballistic missile motion is proposed in order to minimize the estimation errors of the range and range rates incurred by the target´s maneuvers. Considering the estimation errors, the guidance law is designed applying sliding-mode technique in order to deal with the non- maneuvering target and the maneuvering target with imperfect information. Various simulation results can verify the reliability and stability of our designed system.
Keywords :
Kalman filters; missile guidance; reliability; stability; variable structure systems; ballistic missile motion; extended Kalman filter; interacting multiple model technique; missile interception; modified spherical coordinates; passive ranging law; reliability; sliding mode based guidance law; stability; Acceleration; Aerodynamics; Distributed control; Estimation error; Missiles; Navigation; Sliding mode control; Target tracking; USA Councils; Uncertainty;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
American Control Conference (ACC), 2010
Conference_Location :
Baltimore, MD
ISSN :
0743-1619
Print_ISBN :
978-1-4244-7426-4
Type :
conf
DOI :
10.1109/ACC.2010.5531441
Filename :
5531441
Link To Document :
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