2020 American Control Conference (ACC) 2020
DOI: 10.23919/acc45564.2020.9147440
|View full text |Cite
|
Sign up to set email alerts
|

Active Noise Control for Harmonic and Broadband Disturbances Using RLS-Based Model Predictive Control

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
1
1
1

Citation Types

0
11
0

Year Published

2021
2021
2024
2024

Publication Types

Select...
6
2

Relationship

1
7

Authors

Journals

citations
Cited by 12 publications
(11 citation statements)
references
References 16 publications
0
11
0
Order By: Relevance
“…A key goal of the numerical examples is thus to explore manifestations of persistency, consistency, and exigency within OFMPCOI. This article extends the preliminary investigation of OFMPCOI given in [60], [61] through refinements of the control algorithm, more extensive numerical examples, and investigation of persistency, consistency, and exigency.…”
mentioning
confidence: 74%
See 1 more Smart Citation
“…A key goal of the numerical examples is thus to explore manifestations of persistency, consistency, and exigency within OFMPCOI. This article extends the preliminary investigation of OFMPCOI given in [60], [61] through refinements of the control algorithm, more extensive numerical examples, and investigation of persistency, consistency, and exigency.…”
mentioning
confidence: 74%
“…Stabilization of the SISO, chain-of-integrators plants (61) and (62) using u min = −0.1 and u max = 0.1 with and without the move-size control constraint(26), where ∆u min = −0.05 and ∆u max = 0.05. (a) Discrete-time plant(61). Note that, both with and without the move-size control constraint(26), the plant is stabilized by OFMPCOI.…”
mentioning
confidence: 99%
“…where is the moment of inertia relative to c about the ˆ E axis. The longitudinal dynamics of the aircraft are given by ( 13), (14), and (15).…”
Section: Longitudinal Aircraft Dynamicsmentioning
confidence: 99%
“…This paper develops an adaptive flight control system which consists of a nominally tuned total energy control system and an adaptive controller updated by retrospective cost optimization to automate and accelerate the tuning of TECS. The retrospective cost optimization based adaptive control has previously been applied to develop an adaptive autopilot for multicopters [10], [11], adaptive flight control system [12], [13], and active noise control system [14]. The main contribution of this paper is the development of the adaptive TECS and numerical investigation of potential performance improvements.…”
Section: Introductionmentioning
confidence: 99%
“…Therefore, let us assume in the following that a different equalization factor, β k , is desired for each sensor in Figure 2, where the "LMS" block performs the MEFxLMS algorithm. This algorithm selection is not exclusive, so different, and generally more complex, alternative adaptive strategies could be explored, as the recently proposed Recursive Least Squares based Model Predictive Control (RLSMPC) [36] or noiserobust low complexity adaptive schemes like described in [37], [38]. The system needs to know all the pseudo-error noise signals and all the signals that result from filtering the in-phase and quadrature components of the reference signal through their corresponding estimated frequency response of the secondary paths, C jk .…”
Section: Multi-channel Ane For Single-frequency Noisementioning
confidence: 99%