1984
DOI: 10.1115/1.3149673
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Nonlinear Control of Mismatched Uncertain Linear Systems and Application to Control of Aircraft

Abstract: This paper describes an approach to control of nonzero set points of uncertain linear systems based on the theory of ultimate boundedness. We derive a nonlinear control which guarantees that every system response is ultimately bounded within a certain neighborhood of the desired nonzero set point. Analytical expressions for the bounds on variations in parameters for ultimate boundedness are obtained. These results are applied to control of a VTOL aircraft whose time-varying parameters are uncertain. Unlike pre… Show more

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Cited by 56 publications
(19 citation statements)
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“…Consider a linearized model of a helicopter VTOL (vertical take-off and landing) in the vertical plane with airspeed 135 konts [3]. The dynamic equation of this model can be described as respectively.…”
Section: Applicationmentioning
confidence: 99%
See 1 more Smart Citation
“…Consider a linearized model of a helicopter VTOL (vertical take-off and landing) in the vertical plane with airspeed 135 konts [3]. The dynamic equation of this model can be described as respectively.…”
Section: Applicationmentioning
confidence: 99%
“…One typical achievement of these researches is that the state trajectories of the controlled systems can be driven into a bounded region so that the stability of the controlled system is ensured. These researches include [2][3][4][5][6][7].…”
Section: Introductionmentioning
confidence: 99%
“…The original problem here is to find a controller robustly stabilizing the closed-loop system with ρ = 1 and a decay rate of at least α = 0.1. This problem arises in control of helicopters: (Singh and Coelho 1984) and it was studied in Bhattacharyya (1987), El Ghaoui et al (1997), Tempo et al (2004).…”
Section: Stabilizationmentioning
confidence: 99%
“…The given dynamic equation is computed for typical loading and flight conditions of the VTOL helicopter at an airspeed of 135 knots (Singh and Coelho 1984). All the elements of the first three rows of both matrices change as the airspeed changes.…”
Section: Robust Control Of a Vtol Helicoptermentioning
confidence: 99%