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  1. University of Yangon
  2. Department of Physics

Simulation of short range subsonic surface to surface Aerospace Launched vehicle

http://hdl.handle.net/20.500.12678/0000001924
http://hdl.handle.net/20.500.12678/0000001924
ba4daa49-a073-477d-829d-dc0fbba3cdba
ed4e9ee5-0cfd-43dc-bc3d-f9103134c7f4
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Simulation Simulation of short range subsonic surface to surface Aerospace Launched vehicle.pdf (2257 Kb)
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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
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