Dynamics modeling and flight characteristics of folded multi-body aircraft
نویسندگان
چکیده
This paper studies the dynamic modeling method of fold-able multi-body aircraft based on dynamics theory system. Considering as a complete multi-rigid body system, model for free unfolding process after horizontal launch is established. On basis model, coil spring moment and damping flexible connection between flight units are added. Taking certain type three-section wing an example, numerical simulation calculation carried out. The influence stiffness coefficient unit characteristics in deployment relationship maximum initial folding angle studied. Finally, stability envelope determined.
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ژورنال
عنوان ژورنال: Xibei gongye daxue xuebao
سال: 2023
ISSN: ['1000-2758', '2609-7125']
DOI: https://doi.org/10.1051/jnwpu/20234130490