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Abstract

We propose a new algorithm based on interval analysis for design of a robust first order compensator for a jet engine. The proposed algorithm generates the entire set of stabilizing controller parameters. We demonstrate the algorithm on the acceleration control loop of a jet engine in the presence of parametric uncertainties.

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How to Cite
Srivastava, S., Nataraj, P. S. V., & Balakrishnan, S. (2023). Synthesis of A Robustly Stabilizing Compensator for an Uncertain Jet Engine Power Plant. Journal of Aerospace Sciences and Technologies, 58(2), 10–15. https://doi.org/10.61653/joast.v58i2.2006.700

References

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