Uppsats

Precise Trajectory Calculation for Launchers: A MATLAB – Simulink Modeling Approach

Master-uppsats

KTH/Flyg- och rymdteknik, marina system och rörelsemekanik

Publicerad: 2024

Språk: Engelska

Sammanfattning

Optimizing launcher trajectories is essential for effective mission planning, and specialized software like ASTOS provide an initial, precise overview. However, as launcher development progresses, there is a growing need for the creation of an autonomous flight trajectory software that offers greaterflexibility in adjusting simulation parameters and better represents actual, real-life trajectories. Thisreport introduces an initial version of a comprehensive six-degree-of-freedom launcher trajectory calculation software developed using MATLAB and Simulink. The emphasis is on the development strategy, encompassing discussions on dynamics equations, essential features, and crucial models necessary for accurate simulations. Real-world scenarios often deviate from optimized trajectories, and the software addresses these deviations using sensitivity analysis through Monte Carlosimulations, enabling a thorough examination of uncertainties in input parameters and their impact on trajectories. The article delves into the establishment of the dispersion analysis tool and offers suggestions for further enhancements for both the Simulink model and this dispersion analysis tool.

Information

Författare
Barale, Matéo
Lärosäte / institution
KTH/Flyg- och rymdteknik, marina system och rörelsemekanik
Publiceringsdatum
2024
Uppsatstyp
Master-uppsats
Språk
Engelska

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