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H_∞ Hypo-Optimal Control for Spacecraft Orbital Rendezvous

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

  • Published:2000-12-25
  • Supported by:
    国家自然科学基金资助项目! ( 697750 12 )

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.