Wu Tao Yang Yikang Yu Junqi Huang Yongxuan Hu Baosheng (Xi'an Jiaotong University,Xi'an 710049)
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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