2 loop Nonlinear Dynamic Inversion Fuel Flow Controller Design for Air to Air Ducted Ramjet Rocket
نویسندگان
چکیده
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ژورنال
عنوان ژورنال: Defence Science Journal
سال: 2021
ISSN: 0976-464X,0011-748X
DOI: 10.14429/dsj.71.15165