Aircraft Stability Analyzer (ASA)

Aircraft Stability Analyzer allows the user to rapidly analyze the stability of the designed aircraft using the known aerodynamics data.

https://youtu.be/_9WztyL6zkk

이 제출물을 팔로우합니다

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

인용 양식

Joshua Levin Kurniawan (2026). Aircraft Stability Analyzer (ASA) (https://kr.mathworks.com/matlabcentral/fileexchange/163801-aircraft-stability-analyzer-asa), MATLAB Central File Exchange. 검색 날짜: .

일반 정보

MATLAB 릴리스 호환 정보

  • 모든 릴리스와 호환

플랫폼 호환성

  • Windows
  • macOS
  • Linux
버전 퍼블리시됨 릴리스 정보 Action
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