2021
DOI: 10.3390/en14113109
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Control of Optoelectronic Scanning and Tracking Seeker by Means the LQR Modified Method with the Input Signal Estimated Using of the Extended Kalman Filter

Abstract: The paper presents the concept of controlling the designed optoelectronic scanning and tracking seeker. The above device is intended for the so-called passive guidance of short-range anti-aircraft missiles to various types of air maneuvering targets. In the presented control method, the modified linear-quadratic regulator (LQR) and the estimation of input signals using the extended Kalman filter (EKF) were used. The LQR regulation utilizes linearization of the mathematical model of the above-mentioned seeker b… Show more

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Cited by 8 publications
(5 citation statements)
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References 37 publications
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“…(3) The vehicle is mainly subjected to the tire force, ignoring the resistance of air and wind. (4) The vehicle model ignores the pitch angle around the Y-axis and the roll angle around the X-axis 6 . Under the above idealized assumptions, the three-degree-of-freedom dynamics model of the racing is shown in Fig 1.…”
Section: Vehicle Dynamics Modelmentioning
confidence: 99%
“…(3) The vehicle is mainly subjected to the tire force, ignoring the resistance of air and wind. (4) The vehicle model ignores the pitch angle around the Y-axis and the roll angle around the X-axis 6 . Under the above idealized assumptions, the three-degree-of-freedom dynamics model of the racing is shown in Fig 1.…”
Section: Vehicle Dynamics Modelmentioning
confidence: 99%
“…Weight matrix R for two control inputs had the following elements: R = r 11 0 0 r 22 (31) where: r 11 is the weight affecting the first control signal (u 1 ), r 22 is the weight affecting the second control signal (u 2 ). These weights were calculated on the basis of formulas [45]: (32) where: u 1max is the assumed maximum control voltage u 1 , u 2max is the assumed maximum control voltage u 2 .…”
Section: Weight and Covariance Matrixesmentioning
confidence: 99%
“…Gapinski et al presented the concept of controlling the designed optoelectronic tracking and scanning seeker [8]. The device described above is intended for the so-called passive guidance of short-range antiaircraft missiles to various types of air manoeuvring targets.…”
Section: Published Papersmentioning
confidence: 99%