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Simulation of short range subsonic surface to surface Aerospace Launched vehicle
http://hdl.handle.net/20.500.12678/0000001924
http://hdl.handle.net/20.500.12678/0000001924ba4daa49-a073-477d-829d-dc0fbba3cdba
ed4e9ee5-0cfd-43dc-bc3d-f9103134c7f4
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Title | ||||||
Title | Simulation of short range subsonic surface to surface Aerospace Launched vehicle | |||||
Language | en | |||||
Publication date | 2009 | |||||
Authors | ||||||
Hnin Si | ||||||
Saldanha, Clement | ||||||
Zaw Min Naing | ||||||
Description | ||||||
Design methods for guidance system are of significant interest in the launched vehicle flight control community due to their potential for reducing their size for efficiency. In this paper, the launched vehicle's body, stability and dynamics are simulated using RockSim version 5.021 and RocFlight version 3.1. The short range subsonic surface to surface launched vehicle is considered. The vehicle fin deflection response time is calculated with MATLAB. The system in the research work is scale down system to be able to implement. | ||||||
Keywords | ||||||
short range surface to surface launched vehicle | ||||||
Identifier | https://uyr.uy.edu.mm/handle/123456789/309 | |||||
Journal articles | ||||||
Proceedings of the First International Conference on Science and Engineering | ||||||
1 | ||||||
Conference papaers | ||||||
Books/reports/chapters | ||||||
Thesis/dissertations |