摘要
The attitude regulation problem with bounded control for a class of satellites in the presence of large disturbances,with bounded moving average,is solved using a Lyapunov-like design.The analysis and design approaches are introduced in the case in which the underlying system is an integrator and are then applied to the satellite attitude regulation problem.The performance of the resulting closed-loop systems are studied in detail and it is shown that trajectories are ultimately bounded despite the effect of the persistent disturbance.Simulation results on a model of a small satellite subject to large,but bounded in moving average,disturbances are presented.
基金
supported in part by the China Scholarship Council (201906120101)
in part by the European Union’s Horizon 2020 Research and Innovation Program (739551)(KIOS Centre of Excellence)
in part by the Italian Ministry for Research in the framework of the 2017Program for Research Projects of National Interest (PRIN)(2017YKXYXJ)
in part by the Science Center Program of National Natural Science Foundation of China (62188101)
in part by the National Natural Science Foundation of China (61833009, 61690212)
in part by Heilongjiang Touyan Team
