A Satellite Launch Vehicle, during its atmospheric flight, presents a variety of often involve multibody interactions, interactions between the free stream and
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@inproceedings{imav2019:b_theys_et_al, author = {Bart Theys and Joris De Schutter}, editor = {P. Campoy}, title = {Forward flight tests of a quadcopter UAV with various spherical body diameters}, year = {2019}, month = {Sep}, day = {29-04…GitHub - jadnohra/tag_export: An export of my digital library…https://github.com/jadnohra/tag-exportAn export of my digital library (Mathematics, Logic, Physics, Numerical Analysis, Machine Learning, Computer Science) - jadnohra/tag_export
The vehicle's attitude must be taken into account because of its effect on the aerodynamic and propulsive forces. There are other reasons, unrelated to flight dynamics, for controlling the vehicle's attitude in non-powered flight (e.g…
