An approach to integrated guidance/autopilot design for missiles based on the estimations of maneuvering target

An approach to integrated guidance/autopilot design for missiles against maneuvering targets on the sea is studied. When the integrated guidance/autopilot model of the yaw plane is formulated, the guidance/control law is designed based on the backstepping idea and variable structure control theory....

Full description

Saved in:
Bibliographic Details
Main Authors: Jinyong Yu, Yuman Yuan, Youan Zhang, Wenjin Gu
Format: Conference Proceeding
Language:English
Subjects:
Acceleration
Aerospace electronics
Aerospace engineering
Automatic control
Backstepping
Control theory
Coordinate measuring machines
Equations
Missiles
Navigation
Online Access:Request full text
Tags: Add Tag
No Tags, Be the first to tag this record!
Description
Summary:An approach to integrated guidance/autopilot design for missiles against maneuvering targets on the sea is studied. When the integrated guidance/autopilot model of the yaw plane is formulated, the guidance/control law is designed based on the backstepping idea and variable structure control theory. For the unavailable information of the maneuvering target, an estimating method is given. Finally, to verify the effectiveness and rightness of the integrated design scheme, the simulation of some antivessel missile against high maneuvering targets have been made, the simulation results have shown that high accuracy of hitting target can be got.
DOI:10.1109/ICIA.2004.1373316