Numerical state-dependent riccati equation approach for missile integrated guidance control

Journal of Guidance, Control, and Dynamics

Volumn 32, Issue 2, 2009, Pages 699-703

  Vaddi, S S ^a,c   Menon, P K ^a,c   Ohlmeyer, E J ^b,c  

^a OPTIMAL SYNTHESIS INC   (United States)

^b NAVAL SURFACE WARFARE CENTER   (United States)

^c Code G82 ^*  (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIR NAVIGATION; CONSTRAINED OPTIMIZATION; ELECTRONIC GUIDANCE SYSTEMS; EQUATIONS OF STATE; GUIDED MISSILES; NUMERICAL METHODS; RICCATI EQUATIONS;

CLOSED-LOOP SIMULATIONS; CONSTRAINED LEAST SQUARES; INTEGRATED GUIDANCE; KINETIC WARHEADS; MOVING MASS ACTUATED MISSILES; NUMERICAL APPROACHES; STATE-DEPENDENT RICCATI EQUATION; STATE-DEPENDENT SYSTEMS;

INTEGRATION;

EID: 65949085172     PISSN: 07315090     EISSN: 15333884     Source Type: Journal    
DOI: 10.2514/1.34291     Document Type: Article

References (11)

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