Designing an Optimal Control LQT for Controlling and Guidance of Missile
Missile has to be controlled and follow the commanded guidance in order to make its flight hit the target. Since missile has a nonlinear characteristic and coupled dynamic equation, controlling a missile has become more complex. Linear Quadratic Tracking (LQT) is one of optimal control theory where...
| Main Authors: | , , |
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| Format: | Article |
| Language: | English |
| Published: |
Institut Teknologi Sepuluh Nopember
2018-05-01
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| Series: | JAREE (Journal on Advanced Research in Electrical Engineering) |
| Online Access: | http://jaree.its.ac.id/index.php/jaree/article/view/36 |