Aircraft Stability Analyzer (ASA)

版本 1.2.2 (675.5 KB) 作者: Joshua Levin Kurniawan
Aircraft Stability Analyzer allows the user to rapidly analyze the stability of the designed aircraft using the known aerodynamics data.
5.0
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155.0 次下载
更新时间 2024/11/3

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Aircraft Stability Analyzer (ASA) allows the user to rapidly analyze the stability of the designed aircraft using the known aerodynamics data.
This app includes:
1. First order aerodynamics derivative of several preset airplane, including Cessna Model 172, Beech Model 99, SIAI-Marchetti B-211, Gates, Learjet Model 24, McDonnel Douglas F4C, and Boeing 747-100 (Taken from Roskam, Jan. Airplane design. DARcorporation, 1985), or you can define your own aircraft aerodynamics coefficients by manual input or using DATCOM output file,
2. Static stability analysis and compare it to typical aircraft value,
3. Trim triangle analysis,
4. Aircraft trim condition by utilizing Simulink model,
5. Aircraft's linearized equation of motion in a form of state space for both longitudinal and lateral-directional mode,
6. Flight mode (phugoid, short period, dutch roll, spiral, and roll subsidence) analysis.
To learn how to utilize the app, please refer to video link: https://youtu.be/_9WztyL6zkk

引用格式

Joshua Levin Kurniawan (2024). Aircraft Stability Analyzer (ASA) (https://www.mathworks.com/matlabcentral/fileexchange/163801-aircraft-stability-analyzer-asa), MATLAB Central File Exchange. 检索时间: .

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版本 已发布 发行说明
1.2.2

Bug Fixed:
- CL vs alpha and Cm vs alpha issues
- Trimming convergence issues
1.2.1

Bug fixed
1.2

- Moment inertia parameters
- DATCOM .out file example (for reference)
- Several minor bug fixes
1.1