Abstract Guidance law of a homing missile is implemented using an extended high gain observer without the model assumptions on target maneuvers. First, for a class of multi-input–multi-output nonlinear systems, extended high-gain observers are used for output feedback control with partial practical stabilization. Then the method is applied to the guidance law implementation of a homing missile with bearing only measurement. Simulation results show satisfactory performance.
Guidance law implementation with performance recovery using an extended high-gain observer
Aerospace Science and Technology ; 24 , 1 ; 177-186
2011-11-03
10 pages
Article (Journal)
Electronic Resource
English
Guidance law implementation with performance recovery using an extended high-gain observer
Online Contents | 2013
|Recoverable rocket power landing phase guidance method based on extended state observer
European Patent Office | 2023
|Robust Guidance Law with L2 Gain Performance
Online Contents | 2001
|