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POLYNOMIAL FUNCTION BASED GUIDANCE FOR IMPACT ANGLE AND TIME CONTROL
Author(s) -
Tae-Hun Kim
Publication year - 2015
Publication title -
journal of the korea society for industrial and applied mathematics
Language(s) - English
Resource type - Journals
eISSN - 1229-0645
pISSN - 1226-9433
DOI - 10.12941/jksiam.2015.19.305
Subject(s) - missile , polynomial , function (biology) , acceleration , control theory (sociology) , computer science , simple (philosophy) , missile guidance , control (management) , mathematics , mathematical analysis , engineering , artificial intelligence , aerospace engineering , physics , philosophy , epistemology , classical mechanics , evolutionary biology , biology

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