| contributor author | Mostafa Khalil | |
| contributor author | Xiaoting Rui | |
| contributor author | Hossam Hendy | |
| date accessioned | 2017-05-08T21:34:35Z | |
| date available | 2017-05-08T21:34:35Z | |
| date copyright | March 2015 | |
| date issued | 2015 | |
| identifier other | %28asce%29as%2E1943-5525%2E0000384.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/56526 | |
| description abstract | Due 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. | |
| publisher | American Society of Civil Engineers | |
| title | Discrete Time Transfer Matrix Method for Projectile Trajectory Prediction | |
| type | Journal Paper | |
| journal volume | 28 | |
| journal issue | 2 | |
| journal title | Journal of Aerospace Engineering | |
| identifier doi | 10.1061/(ASCE)AS.1943-5525.0000381 | |
| tree | Journal of Aerospace Engineering:;2015:;Volume ( 028 ):;issue: 002 | |
| contenttype | Fulltext | |