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论文类型：期刊论文

发表时间：2013-07-01

发表刊物：SCIENTIFIC WORLD JOURNAL

收录刊物：SCIE、PubMed、Scopus

卷号：2013

页面范围：579703

ISSN号：1537-744X

摘要：The robust H-infinity control for spacecraft rendezvous with a noncooperative target is addressed in this paper. The relative motion of chaser and noncooperative target is firstly modeled as the uncertain system, which contains uncertain orbit parameter and mass. Then the H-infinity performance and finite time performance are proposed, and a robust H-infinity controller is developed to drive the chaser to rendezvous with the non-cooperative target in the presence of control input saturation, measurement error, and thrust error. The linear matrix inequality technology is used to derive the sufficient condition of the proposed controller. An illustrative example is finally provided to demonstrate the effectiveness of the controller.