Neighboring Optimal Guidance and Constrained Attitude Control for Accurate Orbit Injection
نویسندگان
چکیده
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ژورنال
عنوان ژورنال: Aerotecnica Missili & Spazio
سال: 2021
ISSN: 0365-7442,2524-6968
DOI: 10.1007/s42496-021-00077-3