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The paper represents the Kalman Filter based optimal control approach to control the angle of attack of a missile attitude. The Kalman filter is used here to estimate the state of the system. A state feedback Linear Quadratic Gaussian controller which takes the filtered estimated states has been implemented into the system to control the angle of attack of the missile. The proposed method of controller...
This paper proposes the design of continuous and discrete optimal controller based on Continuous and Discrete time Linear Quadratic Regulator (CLQR and DLQR). The controllers have been implemented in Pneumatically Actuated Inverted Pendulum system which is basically non-linear in nature. The main aim is to design the optimal controllers with the given specification for the system and to study the...
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