Short-time stability of proportional navigation guidance loop

IEEE Transactions on Aerospace and Electronic Systems

Volumn 32, Issue 3, 1996, Pages 1107-1115

  Rew, Dong Young ^a,b   Tahk, Min Jea ^a   Cho, Hangju ^a  

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

^b Agency for Defence Development   (South Korea)

Author keywords

[No Author keywords available]

Indexed keywords

ACCELERATION; MISSILES; NAVIGATION; STABILITY CRITERIA; TIME VARYING SYSTEMS;

HOMING GUIDANCE LOOP; PROPORTIONAL NAVIGATION GUIDANCE; SHORT TIME STABILITY CRITERION; STABILITY ANALYSIS;

ELECTRONIC GUIDANCE SYSTEMS;

EID: 0030189975     PISSN: 00189251     EISSN: None     Source Type: Journal    
DOI: 10.1109/7.532269     Document Type: Article

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