Optimal sliding-mode terminal guidance law design of airborne boost-phase ballistic missile interception

Applied Mechanics and Materials

Volumn 40-41, Issue , 2011, Pages 15-20

  Cui, YanKai ^a   Fu, Li ^b   Liang, XiaoGeng ^c   Luo, Ling ^d  

^a NORTHWESTERN POLYTECHNICAL UNIVERSITY   (China)

^b SHAOYANG UNIVERSITY   (China)

^c China Airborne Missile Academy   (China)

^d People's Army of China 5715th Factory ^*  (China)

Author keywords

Ballistic missile; Boost phase interception; Direct hit; Optimal sliding mode; Terminal guidance law

Indexed keywords

BALLISTIC MISSILE; BOOST-PHASE INTERCEPTION; DIRECT HIT; SLIDING MODES; TERMINAL GUIDANCE;

BALLISTIC MISSILES; CONTROL THEORY; DESIGN; EQUATIONS OF MOTION; NAVIGATION; OPTIMIZATION; SYSTEM THEORY;

BALLISTICS;

EID: 78650995359     PISSN: 16609336     EISSN: 16627482     Source Type: Book Series    
DOI: 10.4028/www.scientific.net/AMM.40-41.15     Document Type: Conference Paper

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