Modeling closed-loop control of installation noise using Ginzburg-Landau equation
Ugur Karban, Eduardo Martini, Peter Jordan

TL;DR
This paper develops a Ginzburg-Landau based model to study closed-loop control of aircraft installation noise, comparing causal resolvent control with wave-cancellation, and examining how sensor placement affects control effectiveness.
Contribution
It introduces a simplified yet realistic model for installation noise control, analyzing the impact of causality and sensor placement on control performance.
Findings
Causality constraints reduce control performance when sensors are downstream.
Optimal causal control can mitigate some limitations of causality.
Modeling forcing effects improves control effectiveness.
Abstract
Installation noise is a dominant source associated with aircraft jet engines. Recent studies show that linear wavepacket models can be employed for prediction of installation noise, which suggests that linear control strategies can also be adopted for mitigation of it. We present here a simple model to test different control approaches and highlight the potential restrictions on a successful noise control in an actual jet. The model contains all the essential elements for a realistic representation of the actual control problem: a stochastic wavepacket is obtained via a linear Ginzburg-Landau model; the effect of the wing trailing edge is accounted for by introducing a semi-infinite half plane near the wavepacket; and the actuation is achieved by placing a dipolar point source at the trailing edge, which models a piezoelectric actuator. An optimal causal resolvent-based control method…
Peer Reviews
No public reviews on file for this paper yet. If you reviewed it on a platform where reviews are public (OpenReview, ICLR, NeurIPS, ICML), you can paste yours below so the community can read it here.
Videos
No videos yet. Explain this paper in a talk, walkthrough, or lecture? Add one.
Taxonomy
TopicsProbabilistic and Robust Engineering Design · Aerodynamics and Acoustics in Jet Flows · Acoustic Wave Phenomena Research
