Model predictive control for non-linear missiles

The present paper reports an attempt of applying model predictive control (MPC) to design an autopilot for a non-linear missile. The non-linear, fast dynamics of the missile raise three issues in the design of an MPC algorithm: the choice of the MPC performance index, in particular the terminal weig...

Full description

Saved in:
Bibliographic Details
Main Authors: Xiao-Bing Hu, Wen-Hua Chen
Format: Default Article
Published: 2007
Subjects:
Online Access:https://hdl.handle.net/2134/3757
Tags: Add Tag
No Tags, Be the first to tag this record!