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.
Zitieren als
David Eagle (2024). Aerospace Trajectory Optimization - OTB (https://www.mathworks.com/matlabcentral/fileexchange/73805-aerospace-trajectory-optimization-otb), MATLAB Central File Exchange. Abgerufen .
Kompatibilität der MATLAB-Version
Plattform-Kompatibilität
Windows macOS LinuxKategorien
- Aerospace > Aerospace Blockset > Visualization >
- Sciences > Earth, Ocean, and Atmospheric Sciences > Earth and Planetary Science >
Tags
Community Treasure Hunt
Find the treasures in MATLAB Central and discover how the community can help you!
Start Hunting!Live Editor erkunden
Erstellen Sie Skripte mit Code, Ausgabe und formatiertem Text in einem einzigen ausführbaren Dokument.
Version | Veröffentlicht | Versionshinweise | |
---|---|---|---|
1.0.0 |