2016
DOI: 10.1016/j.ijleo.2016.08.001
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The effect of phantom-bit technology on the performance of phased array seeker detection in the case of the initial beam angle

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Cited by 8 publications
(4 citation statements)
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“…According to the beam control principle [2], design θ = R * θ BC , then θ B = (1 + R * ) θ BC . Moreover, the angular rate gyro scale K g in the missile high-precision inertial navigation system has a small fluctuation range (and can be controlled within the range of 10 −3 during the whole flight), which means K g ∼ = 1.…”
Section: A Mathematical Modelmentioning
confidence: 99%
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“…According to the beam control principle [2], design θ = R * θ BC , then θ B = (1 + R * ) θ BC . Moreover, the angular rate gyro scale K g in the missile high-precision inertial navigation system has a small fluctuation range (and can be controlled within the range of 10 −3 during the whole flight), which means K g ∼ = 1.…”
Section: A Mathematical Modelmentioning
confidence: 99%
“…Hence, the performance of the digital phase shifter determines the performance of the seeker beam scanning. Considering cost and complexity, phantom-bit technology (PBT) is widely applicable in practical engineering [2]. Although PBT can improve seeker beam scanning accuracy, the beam pointing error appears because of the seeker using open-loop control to achieve beam pointing control.…”
Section: Introductionmentioning
confidence: 99%
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“…Furthermore, the phased array radar seeker uses a digital shifter to control the antenna beam pointing but, in principle, this is open-loop control. Even if phantom-bit technology is used to optimally control the beam pointing, it remains impossible to precisely and stably control the beam pointing angle, leading to not only the coupling of the attitude disturbance in the guidance signals but also the coupling with the beam pointing error [7]. Meanwhile, the presence of the radome couples the guidance signals obtained by the seeker with the radome refraction error.…”
Section: Introductionmentioning
confidence: 99%