DocumentCode
438923
Title
Integrated guidance/autopilot scheme for anti-vessel missiles based on three channels independence design idea
Author
Zhao, Guorong ; Xu, Qingjiu ; Yu, Jinyong ; Gu, Wenjin
Author_Institution
Dept. of Autom. Control, Naval Aeronaut. Eng. Inst., Yantai, China
Volume
1
fYear
2004
fDate
6-9 Dec. 2004
Firstpage
778
Abstract
A scheme of integrated guidance/autopilot design for STT missile against maneuvering targets on the sea is proposed. Three channels independence design idea is adopted. Firstly, an integrated guidance/autopilot model of the yaw plane is formulated and the guidance/control law is designed based on the backstepping idea and variable structure control theory. Secondly, control laws are proposed for the height and roll angle, so that when a missile has the capability to hit the target on the yaw plane, and the height approaches zero as the distance between the missile and target on the yaw plane tends to zero, the missile will hit the target. Finally, to verify the effectiveness and rightness of the integrated design scheme, a simulation of some anti-vessel missile against high maneuvering targets was made and the results show that a high accuracy of hitting a target can be achieved.
Keywords
attitude control; control system synthesis; marine vehicles; missile guidance; position control; STT missile; anti-vessel missiles; backstepping; guidance/control law; height control; integrated guidance/autopilot scheme; maneuvering sea targets; roll angle control; three channel independence design; variable structure control theory; yaw plane; Acceleration; Aerospace engineering; Backstepping; Control theory; Coordinate measuring machines; Equations; Missiles; Navigation; Sea measurements; Virtual manufacturing;
fLanguage
English
Publisher
ieee
Conference_Titel
Control, Automation, Robotics and Vision Conference, 2004. ICARCV 2004 8th
Print_ISBN
0-7803-8653-1
Type
conf
DOI
10.1109/ICARCV.2004.1468926
Filename
1468926
Link To Document