NASA's aircraft analysis, design, and optimization tool
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Updated
May 31, 2024 - Python
NASA's aircraft analysis, design, and optimization tool
An open source flight dynamics & control software library
The Loads Kernel Software allows for the calculation of quasi-steady and dynamic maneuver loads, unsteady gust loads in the time and frequency domain as well as dynamic landing loads based on a generic landing gear module.
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Read and write CPACS files. Create an object structure out of CPACS and develop faster.
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