DocumentCode
572508
Title
3D guidance for vertical impact on non-stationary targets
Author
Zhang, Jinpeng ; Cao, Youliang ; Song, Xiaona ; Zhang, Minglian ; Shen, Gongzhang
Author_Institution
Sci. & Technol. on Aircraft Control Lab., Beihang Univ., Beijing, China
fYear
2012
fDate
15-17 Aug. 2012
Firstpage
272
Lastpage
276
Abstract
A new three-dimensional guidance law with high impact angle constraints used for striking ground moving targets is designed based on back-stepping control approach. The kinematics between the missile and the target are established in line-of-sight (LOS) frame. To ensure the required impact angle and small miss distance, two step controllers are designed based on Lyapunov method. The first step controller guarantees the LOS angle in vertical plane to converge to the desired angle. The second step controller can stabilize the overall system while maintaining minimum LOS rate, and thus the smallest miss distance can be achieved indirectly. Simulation results illustrate the efficiency.
Keywords
Lyapunov methods; control system synthesis; missile guidance; 3D guidance; LOS angle; Lyapunov method; back-stepping control approach; designed controller; ground moving targets; high impact angle constraints; line-of-sight frame; miss distance; missile-target kinematics; nonstationary targets; step controller; system stabilization; three-dimensional guidance law; vertical impact; Acceleration; Backstepping; Equations; Missiles; Simulation; Trajectory; Vectors; Air-to-air missiles; Back-stepping control; guidance law; high impact angle; maneuvering target;
fLanguage
English
Publisher
ieee
Conference_Titel
Automation and Logistics (ICAL), 2012 IEEE International Conference on
Conference_Location
Zhengzhou
ISSN
2161-8151
Print_ISBN
978-1-4673-0362-0
Electronic_ISBN
2161-8151
Type
conf
DOI
10.1109/ICAL.2012.6308210
Filename
6308210
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