2018
DOI: 10.1049/iet-cta.2017.0501
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Backstepping‐based zero‐sum differential games for missile‐target interception systems with input and output constraints

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Cited by 30 publications
(16 citation statements)
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“…From (31), we conclude that the optimal control problem has been transformed into the one of obtaining decentralized compensation control laws u i1 , u i2 and decentralized zerosum optimal control law u * i3 , thus, to realize optimal compensation of model uncertainty and collision disturbance of MRM systems.…”
Section: Aci Structure-based Decentralized Zero-sum Optimal Control V...mentioning
confidence: 99%
See 2 more Smart Citations
“…From (31), we conclude that the optimal control problem has been transformed into the one of obtaining decentralized compensation control laws u i1 , u i2 and decentralized zerosum optimal control law u * i3 , thus, to realize optimal compensation of model uncertainty and collision disturbance of MRM systems.…”
Section: Aci Structure-based Decentralized Zero-sum Optimal Control V...mentioning
confidence: 99%
“…In (31), we know that the dynamic model term φ i , the desired joint acceleration term ẍid and the joint velocity error term ėi are all known. In order to compensate these accurately modeled and estimated dynamic model terms, we can design the decentralized compensation control law u i1 as follows:…”
Section: Aci Structure-based Decentralized Zero-sum Optimal Control V...mentioning
confidence: 99%
See 1 more Smart Citation
“…3) In this paper, the strict-feedback system is transformed into an output feedback system firstly, then an adaptive observer is constructed to estimate the states. Compared with [9,20,34,35], this paper does not require the whole states of the system are measurable. For missile guidance systems, the benefit is that it can save space inside the warhead and be equipped with other advanced equipment to enhance the missile's power.…”
Section: Introductionmentioning
confidence: 99%
“…The thought is succeeded for intercepting high-speed manoeuvring targets of interceptor missiles with output and input constraints [24] , and stimulate the choice of optimal ADP zero-sum control strategy for the tracking error dynamics in nonlinear strict-feedback systems.…”
Section: Introductionmentioning
confidence: 99%