Aircraft Design

This app gives all the priliminary data, which helps in optimization of the UAV design

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The following application are present in the app
1.Basic parameter
2. Weight estimation in cruise condition
3.Wing planform selection
4. Airfoil selection
5.Take off performance
6. Climb Performance
7. Cruise Performance
8. Power plant selection
9. Rate of climb
10. Performance parameters
11. Longitudinal Stability
12. Dynamic parameter [should have a transfer function]

引用格式

RAHUL N (2026). Aircraft Design (https://ww2.mathworks.cn/matlabcentral/fileexchange/123245-aircraft-design), MATLAB Central File Exchange. 检索时间: .

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MATLAB 版本兼容性

  • 兼容任何版本

平台兼容性

  • Windows
  • macOS
  • Linux
版本 已发布 发行说明 Action
2.0

Corrected the error in the Climb performance of the UAV

1.0