Aerospace Trajectory Optimization - OTB
Optimization Toolbox version of the MATLAB script that demonstrates aerospace trajectory optimization using direct transcription and collocation. In the language of optimal control theory, this problem is a “continuous system with functions of the state variables prescribed at a fixed terminal time”. The numerical example given in the text is a continuous, low-thrust coplanar orbit transfer from Earth to Mars. The orbits of the planets are assumed to be circular and coplanar, and the total transfer time is about 193 days.
인용 양식
David Eagle (2024). Aerospace Trajectory Optimization - OTB (https://www.mathworks.com/matlabcentral/fileexchange/73805-aerospace-trajectory-optimization-otb), MATLAB Central File Exchange. 검색됨 .
MATLAB 릴리스 호환 정보
플랫폼 호환성
Windows macOS Linux카테고리
- Aerospace > Aerospace Blockset > Visualization >
- Sciences > Earth, Ocean, and Atmospheric Sciences > Earth and Planetary Science >
태그
Community Treasure Hunt
Find the treasures in MATLAB Central and discover how the community can help you!
Start Hunting!버전 | 게시됨 | 릴리스 정보 | |
---|---|---|---|
1.0.0 |