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Data-driven model-free adaptive attitude control of partially constrained combined spacecraft with external disturbances and input saturation 被引量:6

Data-driven model-free adaptive attitude control of partially constrained combined spacecraft with external disturbances and input saturation
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摘要 This study presents an improved data-driven Model-Free Adaptive Control(MFAC)strategy for attitude stabilization of a partially constrained combined spacecraft with external disturbances and input saturation. First, a novel dynamic linearization data model for the partially constrained combined spacecraft with external disturbances is established. The generalized disturbances composed of external disturbances and dynamic linearization errors are then reconstructed by a Discrete Extended State Observer(DESO). With the dynamic linearization data model and reconstructed information, a DESO-MFAC strategy for the combined spacecraft is proposed based only on input and output data. Next, the input saturation is overcome by introducing an antiwindup compensator. Finally, numerical simulations are carried out to demonstrate the effectiveness and feasibility of the proposed controller when the dynamic properties of the partially constrained combined spacecraft are completely unknown. This study presents an improved data-driven Model-Free Adaptive Control(MFAC)strategy for attitude stabilization of a partially constrained combined spacecraft with external disturbances and input saturation. First, a novel dynamic linearization data model for the partially constrained combined spacecraft with external disturbances is established. The generalized disturbances composed of external disturbances and dynamic linearization errors are then reconstructed by a Discrete Extended State Observer(DESO). With the dynamic linearization data model and reconstructed information, a DESO-MFAC strategy for the combined spacecraft is proposed based only on input and output data. Next, the input saturation is overcome by introducing an antiwindup compensator. Finally, numerical simulations are carried out to demonstrate the effectiveness and feasibility of the proposed controller when the dynamic properties of the partially constrained combined spacecraft are completely unknown.
出处 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2019年第5期1281-1293,共13页 中国航空学报(英文版)
基金 supported by National Natural Science Foundation of China(Nos.61603114,61673135) the Fundamental Research Funds for the Central Universities of China(No.HIT.NSRIF.201826)
关键词 Attitude CONTROL COMBINED SPACECRAFT DATA-DRIVEN CONTROL Discrete Extended State Observer(DESO) Input SATURATION Attitude control Combined spacecraft Data-driven control Discrete Extended State Observer(DESO) Input saturation
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