A swarm intelligence based approach has been used for design optimization of a single stage solid propellant small sounding rocket. The selected sounding rocket (SR) is capable of placing a small payload of 20 kg to an apogee of 100 km altitude. This optimization approach combines the advantage of a particle swarm optimization (PSO) to find the optimum. The aerodynamic, trajectory, propulsion and mass model were implemented in a Matlab environment, and a multi feasible design was applied to integrate the modules. It is shown that the proposed optimization approach was able to find a rapid convergence of the optimal solution with acceptable precision.
Multidisciplinary Design Optimization of a Single Stage Sounding Rocket using Swarm Intelligence
11.08.2022
795048 byte
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Two-stage sounding rocket problem
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NTIS | 1967
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AIAA | 1967
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Online Contents | 1995
|