Kalman filter based optimal control approach for attitude control of a missile

Nilanjan Patra, Kaushik Halder, Avijit Routh, Abhro Mukherjee, Satyabrata Das

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Abstract / Description of output

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 takes care of the unwanted noise present in the system and ensures guaranteed convergence of the tracking error to zero as well. The performance of the proposed Kalman filter based controller has been evaluated with the presence of noise and disturbances in the system. Simulation results have been carried out to show the effectiveness of the controller.
Original languageEnglish
Title of host publication2013 International Conference on Computer Communication and Informatics
PublisherIEEE
Pages1-4
Number of pages4
DOIs
Publication statusPublished - 4 Jan 2013
Event2013 International Conference on Computer Communication and Informatics - Coimbatore, India
Duration: 4 Jan 20136 Jan 2013

Conference

Conference2013 International Conference on Computer Communication and Informatics
Abbreviated titleICCCI 2013
Country/TerritoryIndia
CityCoimbatore
Period4/01/136/01/13

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