Optimal guidance laws with terminal impact angle constraint

Journal of Guidance, Control, and Dynamics

Volumn 28, Issue 4, 2005, Pages 724-732

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

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

^b Agency for Defence Development   (South Korea)

^c Department of Aerospace Engineering ^*  (South Korea)

Author keywords

[No Author keywords available]

Indexed keywords

ACCELERATION; ANGLE MEASUREMENT; CALCULATIONS; COMPUTER SIMULATION; FEEDBACK CONTROL; MATRIX ALGEBRA; MISSILES; OPTIMAL CONTROL SYSTEMS;

ANGLE CONSTRAINTS; MISSILE SYSTEMS; OPTIMAL GUIDANCE LAWS; ZERO TERMINALS;

ELECTRONIC GUIDANCE SYSTEMS;

EID: 22944489925     PISSN: 07315090     EISSN: 15333884     Source Type: Journal    
DOI: 10.2514/1.8392     Document Type: Article

References (12)

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