2026-06-24T23:59:23Z https://meral.edu.mm/oai

oai:meral.edu.mm:recid/1924 2021-12-13T05:15:59Z 1582963390870:1582967549708 user-uy

Simulation of short range subsonic surface to surface Aerospace Launched vehicle Hnin Si Saldanha, Clement Zaw Min Naing 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. 2009 http://hdl.handle.net/20.500.12678/0000001924 https://meral.edu.mm/records/1924