Revision as of 23:32, April 30, 2024 view source NoLongerOnTheBall (talk \| contribs) Bureaucrats, Interface administrators, Administrators 2,635 edits Observations/Flat and Nonrotating ← Older edit		Latest revision as of 21:38, June 17, 2024 view source NoLongerOnTheBall (talk \| contribs) Bureaucrats, Interface administrators, Administrators 2,635 edits added Army Research Laboratory - Spinning Projectiles
Line 3: ===Publications=== ====Army Research Laboratory - Spinning Projectiles==== [[File:Mil-projectile_dynamics_2024-06-17_14_31_17.png\|right\|200px]] A 6-DOF rigid projectile model is employed to predict the dynamics of a projectile in flight. These equations assume a flat Earth. The 6-DOF comprises the three translational components describing the position of the projectile’s center of mass and the three Euler angles describing the orientation of the projectile with respect to the Earth. Figures 1 and 2 provide a visualization of the degrees of freedom. [[:File:Army_Research_Labratory_ADA519118.pdf]] ==== American Institute of Aeronautics and Astronautics ==== [[File:General_Equations_of_Motion_for_a_Damaged_Asymmetric_Aircraft.png\|right\|200px]]

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