SCOPUS 정보 검색 플랫폼

ICIC Express Letters

Volumn 4, Issue 5 B, 2010, Pages 1937-1944

Adaptive control for missile systems with parameter uncertainty

(4) Lin, Zhiwei a Zhu, Zheng a Xia, Yuanqing a Wang, Shuo b

a BEIJING INSTITUTE OF TECHNOLOGY (China)

b INSTITUTE OF AUTOMATION (China)

Author keywords

Adaptive control; Back stepping; Missile attitude Control; Sliding mode control

Indexed keywords

ADAPTIVE CONTROL; ADAPTIVE LAWS; CONTROL STRATEGIES; MISSILE SYSTEMS; NON-LINEAR MISSILE; PARAMETER UNCERTAINTY; REFERENCE STATE; SIMULATION RESULT; SLIDING MODE CONTROLLER; SLIDING MODES; STATE VARIABLES;

ATTITUDE CONTROL; CLOSED LOOP SYSTEMS; CONTROL THEORY; MISSILES; NAVIGATION; SLIDING MODE CONTROL; SPATIAL VARIABLES CONTROL; UNCERTAINTY ANALYSIS;

ADAPTIVE CONTROL SYSTEMS;

EID: 77956930206 PISSN: 1881803X EISSN: None Source Type: Journal
DOI: None Document Type: Article

Times cited : (5)

References (8)

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2
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3
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4
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5
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6
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7
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8
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.