2019
DOI: 10.1109/tcst.2017.2761324
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Robust Output Feedback Tracking Control for Inertially Stabilized Platforms With Matched and Unmatched Uncertainties

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Cited by 38 publications
(17 citation statements)
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“…where T i is equivalent inertia time constant, and f d is equivalent friction coefficient. To accurately describe the dynamic characteristics of the ISP, the Stribeck or LuGre friction model is usually used [24], [27]. According to the friction model, we have…”
Section: Dynamic Model Of the Isp Systemmentioning
confidence: 99%
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“…where T i is equivalent inertia time constant, and f d is equivalent friction coefficient. To accurately describe the dynamic characteristics of the ISP, the Stribeck or LuGre friction model is usually used [24], [27]. According to the friction model, we have…”
Section: Dynamic Model Of the Isp Systemmentioning
confidence: 99%
“…Recently ADRC strategy has been applied in ISP control system [22], [23]. And [24] combine ESO and robust control to achieve high-precision tracking control of ISP. In this paper, ADRC will be applied to the stability control of ISP to suppress nonlinear friction, install unbalanced torque, parameter uncertainty and external torque disturbance and to improve the response speed to gyroscope and tracking inputs.…”
Section: Introductionmentioning
confidence: 99%
“…The ISIS isolates nonideal angle disturbances and maintains the line of sight (LOS) of stabilized optical sensors [3]. It is generally affected by disturbance factors, including internal disturbances caused by mass imbalance torque [4], friction torque [5], and cable restraint torque [6], and by external disturbances caused by carrier motion or vibration. Moreover, when environment change occurs, system parameters vary.…”
Section: Introductionmentioning
confidence: 99%
“…In the normal three-axis ISP, the roll, pitch, and yaw gimbals are supported by mechanical bearings and gears [7]. It is possible that the friction of the mechanical bearing and gear affects the attitude stabilization precision of supported gimbals [8][9][10][11]. In addition, the disturbances could be transferred from the pitch and roll gimbals to the yaw gimbal such that the attitude stabilization precision of yaw gimbal is reduced [12][13][14].…”
Section: Introductionmentioning
confidence: 99%