The CEASIOM application is a Conceptual Aircraft design tool. It was developed within the frame of the SimSAC (Simulating Aircraft Stability And Control Characteristics for Use in Conceptual Design) Specific Targeted Research Project (STREP) approved for funding by the European Commission 6th Framework Programme on Research, Technological Development and Demonstration. Work began 1 November 2006 and last 3 years. The SimSAC project aims at significantly enhancing CEASIOM functionality by introducing software that initially focuses on rapid low fidelity analysis, and as appropriate, resort to higher fidelity numerical simulations. Moreover CEASIOM involve stability and control driven sizing and optimization earlier in the design cycle than is standard practice today. CEASIOM runs under either Windows or Linux, and its only requires a MATLAB® license.
Keywords for this software
References in zbMATH (referenced in 2 articles )
Showing results 1 to 2 of 2.
- Siggel, Martin; Kleinert, Jan; Stollenwerk, Tobias; Maierl, Reinhold: TiGL: an open source computational geometry library for parametric aircraft design (2019)
- Vogeltanz, Tomáš: A survey of free software for the design, analysis, modelling, and simulation of an unmanned aerial vehicle (2016)
Further publications can be found at: http://www.ceasiom.com/ceasiom-scientific-publications.html