2014
DOI: 10.1007/978-0-8176-4893-0_8
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Disturbance Observer Based Control: Aerospace Applications

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Cited by 10 publications
(4 citation statements)
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“…The closed-loop stability and convergence of the NLESO are also demonstrated. A proposed extension to this work would include another country with a large population as a case study [ 32 ].…”
Section: Discussionmentioning
confidence: 99%
“…The closed-loop stability and convergence of the NLESO are also demonstrated. A proposed extension to this work would include another country with a large population as a case study [ 32 ].…”
Section: Discussionmentioning
confidence: 99%
“…The Mamdani fuzzy logic system with m inputs, I 1 , …, I m , three outputs, and centre of average defuzzifier is described as [9] F=][1em4ptk=1gj=1mμPjk(Ij)k=1gfalse∏j=1mμPjkfalse(Ijfalse)ω1kk=1gj=1mμPjk(Ij)k=1gfalse∏j=1mμPjkfalse(Ijfalse)ω2kk=1gj=1mμPjk(Ij)k=1gfalse∏j=1mμPjkfalse(Ijfalse)ω3kwhere g is the number of fuzzy rules, pjk is the j th fuzzy set corresponding to the k th fuzzy rule, μPjk is the membership function of the fuzzy set …”
Section: Fuzzy Approximationmentioning
confidence: 99%
“…Recently, several non‐linear control techniques have been proposed for aerial flight, such as feedback linearisation, non‐linear dynamic inversion [57], sliding mode control [8, 9] and adaptive control techniques utilising back‐stepping and super‐twisting methods [1013]. In [5], the original non‐linear dynamic system is transformed into a linear system by coordinate transformation and state feedback.…”
Section: Introductionmentioning
confidence: 99%
“…. The term α is calculated from the reachability conditionσσ ≤ − α √ 2 |σ| and the term L equals the maximum value of Φ(x 1 ,x 2 ) = A 1x1 + A 2x2 (Shtessel et al, 2014).…”
Section: Appendix Bmentioning
confidence: 99%