Closed-form optimal guidance law for missiles of time-varying velocity

Journal of Guidance, Control, and Dynamics

Volumn 19, Issue 5, 1996, Pages 1017-1022

  Cho, Hangju ^a   Ryoo, Chang Kyung ^a   Tahk, Min Jea ^b,c  

^a Agency for Defence Development   (South Korea)

^b Korea Advanced Institute of Science and Technology (KAIST)   (South Korea)

^c AIAA ^*

Author keywords

[No Author keywords available]

Indexed keywords

CALCULATIONS; COMPUTER SIMULATION; ELECTRONIC GUIDANCE SYSTEMS; EQUATIONS OF MOTION; GEOMETRY; LINEARIZATION; MISSILES; TIME VARYING SYSTEMS; VECTORS;

CLOSED FORM OPTIMAL GUIDANCE LAW; OPTIMAL GUIDANCE LAWS; PROPORTIONAL NAVIGATION GUIDANCE;

OPTIMAL CONTROL SYSTEMS;

EID: 0030242427     PISSN: 07315090     EISSN: 15333884     Source Type: Journal    
DOI: 10.2514/3.21740     Document Type: Article

References (7)

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