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NASA NTRS ยท 20030067930

Genetic Algorithm Tuned Fuzzy Logic for Gliding Return Trajectories

Abstract

The problem of designing and flying a trajectory for successful recovery of a reusable launch vehicle is tackled using fuzzy logic control with genetic algorithm optimization. The plant is approximated by a simplified three degree of freedom non-linear model. A baseline trajectory design and guidance algorithm consisting of several Mamdani type fuzzy controllers is tuned using a simple genetic algorithm. Preliminary results show that the performance of the overall system is shown to improve with genetic algorithm tuning.

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BibTeXRIS

Burchett, Bradley T.. 2003-01-01. Genetic Algorithm Tuned Fuzzy Logic for Gliding Return Trajectories. https://ntrs.nasa.gov/citations/20030067930

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