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1.
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The paper presents a method of controlling a gyroscope system constituting a drive in observation and tracking heads and in the coordinator of the target of self-guiding [...]
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2.
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The paper reports a control algorithm for air-to-ground missile that performs a pre-programmed flight along an ellipse section. The control system of the object flight is [...]
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3.
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The paper presents a numerical selection method for PID controller gains used for controlling cannons azimuth and elevation angles in the modified artillery and missile s [...]
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4.
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The paper presents the modifications of missile control actuation systems. The control actuation system was modified by adding a swiveling nozzle of the rocket engine. In [...]
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5.
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An algorithm of the gyroscope system control in the seeker with the use of LQR (linear quadratic regulator) modified method was presented in this paper. The modification [...]
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6.
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Precision of anti-aircraft missile homing depends mainly on correct determination of the current angle between the axis of the gyroscope system and the line of sight. The [...]
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