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Cambridge Rocketry Simulator v3.0

Cambridge Rocketry Simulator v3.0
Cambridge Rocketry Simulator v3.0
The third version of the Cambridge Rocketry Simulator consists of three parts to simulating a high power rocket flight. First the user is able to build a rocket from basic components using a GUI. Second, a verified and reviewed physics model simulates the rocket flight, this includes a Monte Carlo wrapper to quantify the uncertainty in dynamics and atmosphere. Finally, the visualization of the resulting trajectories includes nominal performance and uncertainty analysis, e.g. a splash-down region with confidence bounds. The project is available on SourceForge, and is written in Java (GUI), \CC (simulation core) and Python (visualization). While all parts can be executed from the GUI, the three components share information via XML, accommodating modifications, and re-use of individual components. The software can used to simulate the flight of unguided rockets, with both design and operational applications.
Zenodo
Eerland, Willem
7f5826c3-536f-4fdc-955e-0f9870c96a0e
Box, Simon
2bc3f3c9-514a-41b8-bd55-a8b34fd11113
Eerland, Willem
7f5826c3-536f-4fdc-955e-0f9870c96a0e
Box, Simon
2bc3f3c9-514a-41b8-bd55-a8b34fd11113

(2016) Cambridge Rocketry Simulator v3.0. Zenodo doi:10.5281/zenodo.53994 [Software]

Record type: Software

Abstract

The third version of the Cambridge Rocketry Simulator consists of three parts to simulating a high power rocket flight. First the user is able to build a rocket from basic components using a GUI. Second, a verified and reviewed physics model simulates the rocket flight, this includes a Monte Carlo wrapper to quantify the uncertainty in dynamics and atmosphere. Finally, the visualization of the resulting trajectories includes nominal performance and uncertainty analysis, e.g. a splash-down region with confidence bounds. The project is available on SourceForge, and is written in Java (GUI), \CC (simulation core) and Python (visualization). While all parts can be executed from the GUI, the three components share information via XML, accommodating modifications, and re-use of individual components. The software can used to simulate the flight of unguided rockets, with both design and operational applications.

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More information

Published date: 2016

Identifiers

Local EPrints ID: 473242
URI: http://eprints.soton.ac.uk/id/eprint/473242
PURE UUID: c7687d15-2bc5-4a18-9a5d-c9d0788b0261
ORCID for Willem Eerland: ORCID iD orcid.org/0000-0002-4559-6122

Catalogue record

Date deposited: 12 Jan 2023 18:15
Last modified: 17 Mar 2024 00:10

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Contributors

Author: Willem Eerland ORCID iD
Author: Simon Box

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