LPV controller synthesis for a generic missile model

The paper presents an example of a linear, parameter varying (LPV) controller synthesis for a generic nonlinear missile. It is based on obtaining a parameter dependent Ljapunov function, in order to ensure stability of the system. The LPV model of the missile is constructed by means of Jacobian line...

Full description

Saved in:
Bibliographic Details
Main Authors: Pfifer, Harald, Hecker, Simon
Format: Conference Proceeding
Language:English
Subjects:
Actuators
Mathematical model
Missiles
Optimization
Robustness
Sensors
Online Access:Request full text
Tags: Add Tag
No Tags, Be the first to tag this record!
Description
Summary:The paper presents an example of a linear, parameter varying (LPV) controller synthesis for a generic nonlinear missile. It is based on obtaining a parameter dependent Ljapunov function, in order to ensure stability of the system. The LPV model of the missile is constructed by means of Jacobian linearization at fixed parameter values. Performance requirements of the control system are specified in an induced L 2 -norm framework, which is similar to the H ∞ -synthesis in the linear time invariant (LTI) case. The suitable weighting functions are found using a multi-objective optimization approach. Finally, the LPV controller is assessed by a comparison to a classical PI controller.
ISSN:1085-1992
2576-3210
DOI:10.1109/CCA.2010.5611127