Nonsingular terminal sliding mode control for reusable launch vehicle with atmospheric disturbances
2017 ◽
Vol 232
(11)
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pp. 2019-2033
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Keyword(s):
The controller design for reusable launch vehicles is challenging due to enormous amounts of model parameter uncertainties and atmospheric disturbances. This paper first derives six-degree-of-freedom model of a reusable launch vehicle with atmospheric disturbances. Next, four kinds of atmospheric disturbances are introduced and wind models are established respectively. For attitude control of the reusable launch vehicle, a nonsingular terminal sliding mode controller is designed with stability guaranteed. Finally, simulation results show a satisfactory performance for the attitude tracking of the reusable launch vehicle with atmospheric disturbances.
2018 ◽
Vol 76
◽
pp. 14-26
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Keyword(s):
2021 ◽
Vol ahead-of-print
(ahead-of-print)
◽
2018 ◽
Vol 25
(5)
◽
pp. 1008-1018
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2014 ◽
Vol 7
(1)
◽
pp. 95-110
◽
2018 ◽
Vol 233
(11)
◽
pp. 4141-4153
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