Modeling and Simulating Guidance Laws for Gun-Launched Guided Munitions | ||||
| International Conference on Aerospace Sciences and Aviation Technology | ||||
| Article 70, Volume 13, AEROSPACE SCIENCES & AVIATION TECHNOLOGY, ASAT- 13, May 26 – 28, 2009, May 2009, Page 1-13 PDF (286.69 K) | ||||
| Document Type: Original Article | ||||
| DOI: 10.21608/asat.2009.23744 | ||||
 View on SCiNiTO | ||||
| Author | ||||
| Hatem H. Daken | ||||
| Ph.D., Senior Structural Analysis Scientist/Engineer, Boeing Commercial Airplanes, The Boeing Company, Seattle, WA, USA (work was performed while working as the Principal Engineer, Defense Technology Inc., DTI, Arlington, VA, USA). | ||||
| Abstract | ||||
| Models for selected guidance laws were designed and built using The Mathworks’ SIMULINK. These guidance law blocks were used in an exterior ballistics model to evaluate the feasibility of utilizing body fixed seekers for shipboard gun-launched guided munitions based on the kinematic capability of candidate munitions to intercept and destroy highly maneuvering surface targets at close ranges and from different directions. | ||||
| Keywords | ||||
| SIMULINK; Guided Munitions; Guidance Blocks; Body-Fixed Seekers | ||||
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