2015
DOI: 10.1016/j.cja.2015.10.005
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A systematic method of smooth switching LPV controllers design for a morphing aircraft

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Cited by 52 publications
(34 citation statements)
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“…A multiloop control structure comprised of linear inner-loop and outer-loop controller is proposed for a kind of folding-wing aircraft [4]; similarly, the idea can also be found in [1] depending on gain self-scheduled ∞ technique. Subsequently, a finite-time boundedness control approach [2] and a switching linear parameter varying method [6] are investigated for swept-back wing aircraft, respectively. The common feature in [1,2,4,6] is that the controllers are capable of ensuring the aircraft flight steady subject to the wing shape changes, but those designs are highly dependent on the precise prior knowledge of the dynamic model.…”
Section: Introductionmentioning
confidence: 99%
See 1 more Smart Citation
“…A multiloop control structure comprised of linear inner-loop and outer-loop controller is proposed for a kind of folding-wing aircraft [4]; similarly, the idea can also be found in [1] depending on gain self-scheduled ∞ technique. Subsequently, a finite-time boundedness control approach [2] and a switching linear parameter varying method [6] are investigated for swept-back wing aircraft, respectively. The common feature in [1,2,4,6] is that the controllers are capable of ensuring the aircraft flight steady subject to the wing shape changes, but those designs are highly dependent on the precise prior knowledge of the dynamic model.…”
Section: Introductionmentioning
confidence: 99%
“…Subsequently, a finite-time boundedness control approach [2] and a switching linear parameter varying method [6] are investigated for swept-back wing aircraft, respectively. The common feature in [1,2,4,6] is that the controllers are capable of ensuring the aircraft flight steady subject to the wing shape changes, but those designs are highly dependent on the precise prior knowledge of the dynamic model. However, the aerodynamic forces and moments are also quite difficult to model accurately.…”
Section: Introductionmentioning
confidence: 99%
“…Due to the significant wing reconfiguration, aerodynamic parameters, which are varied dramatically, will make the morphing aircraft be a complicated system with strong nonlinearity and uncertainties. Therefore, analysis and control of morphing aircraft are more challenging than those for traditional flight vehicles [10,15]. On the other hand, compared with conventional wing-fixed aircraft, the morphing aircraft has multi-objective adaptability, wider flight envelop and higher combat effectiveness [4].…”
Section: Introductionmentioning
confidence: 99%
“…[14], a switching LPV controller is used to regulate the air-fuel ratio of an internal combustion engine, and all of them have improved system performance in certain extent. Meanwhile, for the purpose of improving design performance and transient responses as switching occurs, a smooth switching strategy has also been developed and various successful control applications have been reported [5,6,10].…”
Section: Introductionmentioning
confidence: 99%
“…Separation methods can clarify multiple factors, or peaks in a single run, therefore such means can be treated as multidimensional information providing methods [6]. Among them capillary electrophoresis, gas chromatography and liquid chromatography are dominating in phytochemical investigations [7,8]. Capillary electrophoresis is a method that is used for separation of soluble charged, or chargeable analytes [9].…”
Section: Introductionmentioning
confidence: 99%