Article ID | Journal | Published Year | Pages | File Type |
---|---|---|---|---|
1718328 | Aerospace Science and Technology | 2013 | 10 Pages |
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.
Related Topics
Physical Sciences and Engineering
Engineering
Aerospace Engineering
Authors
Kemao Ma, Hassan K. Khalil, Yu Yao,