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Wu Tao Yang Yikang Yu Junqi Huang Yongxuan Hu Baosheng (Xi'an Jiaotong University,Xi'an 710049)
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Abstract: The problem of control for two spacecrafts rendezvous is investigated.The method is presented that orbital design uses optimal control method and controller is gotten by H ∞ control means.The method is validated by a simulation example.The method has robust control effect and hypo-optimal orbital character.The results provide the practicable method for the engineering design of spacecraft rendezvous.
Wu Tao Yang Yikang Yu Junqi Huang Yongxuan Hu Baosheng (Xi'an Jiaotong University,Xi'an 710049). H_∞ Hypo-Optimal Control for Spacecraft Orbital Rendezvous[J]. .
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