This paper presents a method of controlling an anti-ship missile with the use of the linear-quadratic regulator (LQR). The equations of dynamics of the flight were linearized and written in the form of equations of state. To control the anti-ship missile, a double executive gas-dynamic (moveable nozzle of exhaust gases) and aerodynamic (moveable control surfaces) system is applied. The missile flight is considered in a three dimensional space, whereas the controlling vector is comprised of four components: two components to control the height of the flight and two components to control the direction of the flight. The results are presented in a graphic form.
Optimal Compensator for Anti-Ship Missile with Vectorization of Engine Thrust
Applied Mechanics and Materials ; 817 ; 279-288
2016-01-05
10 pages
Article (Journal)
Electronic Resource
English
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