We present two alternative observer-based H-infinity control design methods for linear dynamic systems with delay in the state. Based on the Riccati-equation approach, we design observer-based feedback control laws that guarantee the asymptotic stability if the closed-loop control system and reduce the effect of the disturbance input on the controlled output to a prescribed level. Copyright (C) 1996 Elsevier Science Ltd.
机构:
NASA,LYNDON B JOHNSON SPACE CTR,DIV NAVIGAT CONTROL & AERONAUT,HOUSTON,TX 77058NASA,LYNDON B JOHNSON SPACE CTR,DIV NAVIGAT CONTROL & AERONAUT,HOUSTON,TX 77058
WANG, YJ
SHIEH, LS
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机构:
NASA,LYNDON B JOHNSON SPACE CTR,DIV NAVIGAT CONTROL & AERONAUT,HOUSTON,TX 77058NASA,LYNDON B JOHNSON SPACE CTR,DIV NAVIGAT CONTROL & AERONAUT,HOUSTON,TX 77058
SHIEH, LS
SUNKEL, JW
论文数: 0引用数: 0
h-index: 0
机构:
NASA,LYNDON B JOHNSON SPACE CTR,DIV NAVIGAT CONTROL & AERONAUT,HOUSTON,TX 77058NASA,LYNDON B JOHNSON SPACE CTR,DIV NAVIGAT CONTROL & AERONAUT,HOUSTON,TX 77058
机构:
NASA,LYNDON B JOHNSON SPACE CTR,DIV NAVIGAT CONTROL & AERONAUT,HOUSTON,TX 77058NASA,LYNDON B JOHNSON SPACE CTR,DIV NAVIGAT CONTROL & AERONAUT,HOUSTON,TX 77058
WANG, YJ
SHIEH, LS
论文数: 0引用数: 0
h-index: 0
机构:
NASA,LYNDON B JOHNSON SPACE CTR,DIV NAVIGAT CONTROL & AERONAUT,HOUSTON,TX 77058NASA,LYNDON B JOHNSON SPACE CTR,DIV NAVIGAT CONTROL & AERONAUT,HOUSTON,TX 77058
SHIEH, LS
SUNKEL, JW
论文数: 0引用数: 0
h-index: 0
机构:
NASA,LYNDON B JOHNSON SPACE CTR,DIV NAVIGAT CONTROL & AERONAUT,HOUSTON,TX 77058NASA,LYNDON B JOHNSON SPACE CTR,DIV NAVIGAT CONTROL & AERONAUT,HOUSTON,TX 77058