2013
DOI: 10.1007/s11768-013-1164-5
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Second-order terminal sliding mode control for hypersonic vehicle in cruising flight with sliding mode disturbance observer

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Cited by 42 publications
(27 citation statements)
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“…At the same time, AW is employed to suppress actuators' input saturation. The superior 520 performance of this control approach is verified by numerical simulations compared with the previous works (Jiang et al 521 2015; Zhang et al 2013). In order to obtain a more practical attitude control performance, the RCS control allocation 522 logic and the thrusters' configuration of Mars entry vehicle should be more carefully considered.…”
mentioning
confidence: 55%
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“…At the same time, AW is employed to suppress actuators' input saturation. The superior 520 performance of this control approach is verified by numerical simulations compared with the previous works (Jiang et al 521 2015; Zhang et al 2013). In order to obtain a more practical attitude control performance, the RCS control allocation 522 logic and the thrusters' configuration of Mars entry vehicle should be more carefully considered.…”
mentioning
confidence: 55%
“…479 In the fourth case, the hybrid SMDO-TSMC-AW algorithm is adopted to track the reference attitude profile. The 502 SMC and super-twisting SMDO approaches mentioned in references (Zhang et al 2013 are employed 503 in this simulation case for performance comparison. As expected, the attitude tracking control process for Mars entry 504 vehicle in the presence of both model uncertainties and external disturbances has the best performance than the three 505 cases above, just as shown in Fig.5.…”
Section: Super-twisting Sliding Mode Disturbance Observer Design 304mentioning
confidence: 99%
“…In [33,34], composite control design procedures of the disturbance-observer-based controller and TSMC are o ered for the uncertain structural and nonlinear systems where the proposed disturbance observers are based on the regional pole placement and D-stability theories. In [37], by combining TSMC and second-order SMC approaches, a nonlinear robust control technique and a disturbance observer are designed for the longitudinal dynamics of hypersonic vehicles with uncertainties and disturbances, which can provide high-precision and fast convergence.…”
Section: Literature Reviewmentioning
confidence: 99%
“…In [22], a sliding mode disturbance observer with switching-gain adaptation was proposed. In [23,24], the second-order sliding mode disturbance observer, which can produce continuous estimation signals and possess strong robustness, had been proposed and applied to industrial systems.…”
Section: Introductionmentioning
confidence: 99%