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contributor authorMostafa Khalil
contributor authorXiaoting Rui
contributor authorHossam Hendy
date accessioned2017-05-08T21:34:35Z
date available2017-05-08T21:34:35Z
date copyrightMarch 2015
date issued2015
identifier other%28asce%29as%2E1943-5525%2E0000384.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/56526
description abstractDue to the importance of the ballistic trajectory computation including the estimation of launch point and impact point problems, a fast and accurate model is needed to increase the weapon precession. A discrete time transfer matrix method is developed and presented in this paper to compute the trajectory for both fin- and spin-stabilized artillery projectiles. This method is based on discretizing the projectile continuous nonlinear system into a set of linear equations using a second-order Taylor series. These equations are collected into one transfer matrix which can be used in trajectory prediction with high computation speed by evaluating a set of algebraic equations instead of integrating differential equations. Results demonstrate that the presented formulation agrees very well with those obtained numerically using the well-known nonlinear 6-degree-of-freedom model.
publisherAmerican Society of Civil Engineers
titleDiscrete Time Transfer Matrix Method for Projectile Trajectory Prediction
typeJournal Paper
journal volume28
journal issue2
journal titleJournal of Aerospace Engineering
identifier doi10.1061/(ASCE)AS.1943-5525.0000381
treeJournal of Aerospace Engineering:;2015:;Volume ( 028 ):;issue: 002
contenttypeFulltext


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