Optimal Control and Output Feedback Considerations for Missile with Blended Aero-fin and Lateral Impulsive Thrust
نویسندگان
چکیده
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ژورنال
عنوان ژورنال: Chinese Journal of Aeronautics
سال: 2010
ISSN: 1000-9361
DOI: 10.1016/s1000-9361(09)60234-x