Closed-form solutions of optimal guidance with terminal impact angle constraint

IEEE Conference on Control Applications - Proceedings

Volumn 1, Issue , 2003, Pages 504-509

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

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

^b Agency for Defence Development   (South Korea)

Author keywords

Impact angle control; Optimal guidance; Time to go estimation

Indexed keywords

ACCELERATION; CALCULATIONS; COMPUTER SIMULATION; MISSILES; OPTIMAL CONTROL SYSTEMS; PARAMETER ESTIMATION; POLYNOMIALS; TIME VARYING CONTROL SYSTEMS;

IMPACT ANGLE CONTROL; LINEAR TIME VARYING; OPTIMAL GUIDANCE; TIME-TO-GO CALCULATION;

ELECTRONIC GUIDANCE SYSTEMS;

EID: 0344927121     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (10)

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