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
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;
Conference_Titel :
Automation and Logistics (ICAL), 2012 IEEE International Conference on
Conference_Location :
Zhengzhou
Print_ISBN :
978-1-4673-0362-0
Electronic_ISBN :
2161-8151
DOI :
10.1109/ICAL.2012.6308210