2015
DOI: 10.1049/iet-cta.2015.0178
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Smooth switching linear parameter‐varying control for hypersonic vehicles via a parameter set automatic partition method

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Cited by 18 publications
(9 citation statements)
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“…Since lim t → ∞ ζ 2 ℐ (t) = d ℐ (t) and S ϑ is a Hurwitz matrix, it is concluded that lim t → ∞ ζ 2 (t) = d (t). Also, since lim t → ∞ ζ 2 (t) = d (t), the system represented by (27) is a special case of the system (14). The rest of the proof is similar to proof of Lemma 1.…”
Section: E C D G R T}mentioning
confidence: 74%
See 1 more Smart Citation
“…Since lim t → ∞ ζ 2 ℐ (t) = d ℐ (t) and S ϑ is a Hurwitz matrix, it is concluded that lim t → ∞ ζ 2 (t) = d (t). Also, since lim t → ∞ ζ 2 (t) = d (t), the system represented by (27) is a special case of the system (14). The rest of the proof is similar to proof of Lemma 1.…”
Section: E C D G R T}mentioning
confidence: 74%
“…The presence of non-linearities in the system dynamics is another challenging issue for the control design problem in multiagent systems. Furthermore, in many practical multi-agents applications, the agents often exhibit time varying dynamics due to the variation in endogenous or exogenous parameters [24][25][26][27][28]. Stability analysis and control design problems for linear parametervarying (LPV) systems have been studied to cope with the nonlinearities of such physical systems.…”
Section: Introductionmentioning
confidence: 99%
“…The LPV controller operates over the whole range of flight conditions without having to create a scheduling scheme. There are several researches applied LPV control method to fixed-wing aircraft [86][87][88][89][90][91], and few investigations are conducted on rotorcrafts [92,93] because of the following reasons: (1) the nonlinear helicopter model is not affine in control inputs because of the mainrotor dynamics; (2) the rapid variation of flight parameters requires fast transient response, which provides rigorous constraints for controller synthesis; (3) the selection of effective scheduling variables is challenging, since inner dynamics, such as inflow dynamics and blade flapping dynamics, have to be considered.…”
Section: Other Modern Control Methodologies Lqr/lqg Andmentioning
confidence: 99%
“…For each subregion, one local LPV controller is designed and switching among local controllers is performed according to switching laws such as hysteresis, average-dwell-time (ADT), and smooth switching methods. 19,[25][26][27][28] State-dependent switching without online measurement of varying parameters and also using online measurement of scheduling parameters are considered in the presented methods by Deaecto et al 29 and by Yang et al, 30,31 respectively. Simultaneous design of switching surfaces and a switching LPV controller is tackled in some works.…”
Section: Introductionmentioning
confidence: 99%