2017
DOI: 10.1002/asjc.1495
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Attitude Tracking Control of A Quad‐Rotor with Partial Loss of Rotation Effectiveness

Abstract: This paper investigates the attitude control problem of a quad‐rotor unmanned helicopter. In response to adverse factors, including the lumped disturbance, inertia parameter uncertainties, and the partial loss of rotation effectiveness, an adaptive compensation control strategy combining the terminal sliding mode technique and the input shaping method is proposed. Specifically, a group of updating laws using an adaptive mechanism is added to adjust the control strategy in a manner conductive to attitude stabil… Show more

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Cited by 17 publications
(26 citation statements)
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“…is the combined vector of the unknown entries in −1 (k − 1) and E(k), A T (k − 1) ∈  mn×(n+1)m is the known matrix of coefficients with the entries associated to −1 (k − 1) and E(k) in (17). It is readily to get a suitable solution of (18) by the numerical algebra matrix theory.…”
Section: State Estimator Design To Tolerate Sensor Faultsmentioning
confidence: 99%
See 1 more Smart Citation
“…is the combined vector of the unknown entries in −1 (k − 1) and E(k), A T (k − 1) ∈  mn×(n+1)m is the known matrix of coefficients with the entries associated to −1 (k − 1) and E(k) in (17). It is readily to get a suitable solution of (18) by the numerical algebra matrix theory.…”
Section: State Estimator Design To Tolerate Sensor Faultsmentioning
confidence: 99%
“…In recent years, the FTC design emphasized on the control performance and physical constraints like the actuator saturation has been studied besides the closed-loop stability, see e.g. [10][11][12][13][14][15][16][17][18]. Indeed, it is practical and very intractable in developing FTC strategy with the performance requirement and system input and output (I/O) constraints from the limitations on physical components, operating circumstance and product quality.…”
Section: Introductionmentioning
confidence: 99%
“…we try to find bounded input d (t) to track d (t) precisly for system (2). The lifting technique [22] is applied to transform the time-varying system (2) into an equivalent time-invariant system.…”
Section: System Reconstructionmentioning
confidence: 99%
“…For system (2), our goal is to find the control input d (t) so as to get (t) = d (t) for t ∈ [0, ∞).…”
Section: Singular Case (B)mentioning
confidence: 99%
“…It has a robust behavior in the presence of disturbances and uncertainties. [1][2][3][4][5] Furthermore, it has been recently employed in the case of constrained nonlinear systems. 6 While SMC is a simple approach to robust control, 7 implementing this method for designing controllers is more difficult.…”
Section: Introductionmentioning
confidence: 99%