2018
DOI: 10.1177/0954410017748968
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Active disturbance rejection guidance and control scheme for homing missiles with impact angle constraints

Abstract: An active disturbance rejection guidance and control scheme for homing missiles with three-dimensional impact angle constraints is proposed. The six-degree-of-freedom dynamical and kinematical models containing model uncertainties and disturbances are established. A strict feedback relative dynamics between the target and homing missile in three-dimensional space are deduced. A reconstructed reduced-order attitude controller design model is proposed. A two-loop control structure with respect to the centroid gu… Show more

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Cited by 4 publications
(2 citation statements)
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“…ADRC provides a new paradigm for traditional control problems, that is, actively estimating and eliminating internal and external disturbances. With the natural advantage of anti-interference, it has been widely used in motor control [22], [23], robot arm servo control [24], [25], spacecraft flight control [26]- [28], power system control [29]- [32], missile control [33], [34], and other fields and has been highly concerned by control theorists [35]- [41]. Soudbakhsh et al [42] compared the linear optimal method with the sliding-mode variable structure control method, and tracked the mobile robot at low speed and high speed.…”
Section: Introductionmentioning
confidence: 99%
“…ADRC provides a new paradigm for traditional control problems, that is, actively estimating and eliminating internal and external disturbances. With the natural advantage of anti-interference, it has been widely used in motor control [22], [23], robot arm servo control [24], [25], spacecraft flight control [26]- [28], power system control [29]- [32], missile control [33], [34], and other fields and has been highly concerned by control theorists [35]- [41]. Soudbakhsh et al [42] compared the linear optimal method with the sliding-mode variable structure control method, and tracked the mobile robot at low speed and high speed.…”
Section: Introductionmentioning
confidence: 99%
“…To achieve the desired terminal impact angle, a new IGC law is proposed for a homing missile [32]. In order to intercept the ground fixed target and ground maneuvering target, a new IGC law is investigated for a STT homing missile with impact angle constraints [33]. Also in [34], a new robust 3-D IGC method cater to impact angle constraints is designed for STT hypersonic missile with high uncertainties.…”
Section: Introductionmentioning
confidence: 99%