Direct Multi‐Thread Adaptive Control With Attracting Manifold Design

ABSTRACT This article presents a novel multi‐thread attracting manifold (MTAM) adaptive control scheme. The novel contribution of this new controller lies in how the attracting manifold design method is spread across multiple estimates of the truth while simultaneously weighting between said individual estimates to arrive at an adaptive composite estimate which outperforms single thread adaptive controllers. A notable benefit of this new formulation is that it allows for both the weighting of multiple threads and monotonic decrease of parameter error to aid the performance of transient error dynamics, without arbitrarily increasing adaptation gains. The benefits of the proposed controller over existing adaptive control schemes are analyzed through two aerospace flight control applications from the literature.

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Publication Details

Journal
International Journal of Adaptive Control and Signal Processing
Published
2024-10-23
DOI
https://doi.org/10.1002/acs.3920
Citations
1
Primary Topic
Control Systems and Identification
Type
article
Field-Weighted Citation Impact
0.33

Funders

Controls
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article

Direct Multi‐Thread Adaptive Control With Attracting Manifold Design

Maruthi Ram Akella, Richard D. Hoobler
1 citations
International Journal of Adaptive Control and Signal Processing
Control Systems and Identification
0.33
article

Direct Multi‐Thread Adaptive Control With Attracting Manifold Design

Maruthi Ram Akella, Richard D. Hoobler
article en
1 citations

Abstract

ABSTRACT This article presents a novel multi‐thread attracting manifold (MTAM) adaptive control scheme. The novel contribution of this new controller lies in how the attracting manifold design method is spread across multiple estimates of the truth while simultaneously weighting between said individual estimates to arrive at an adaptive composite estimate which outperforms single thread adaptive controllers. A notable benefit of this new formulation is that it allows for both the weighting of multiple threads and monotonic decrease of parameter error to aid the performance of transient error dynamics, without arbitrarily increasing adaptation gains. The benefits of the proposed controller over existing adaptive control schemes are analyzed through two aerospace flight control applications from the literature.

International Journal of Adaptive Control and Signal ProcessingVol. 39(1)
The University of Texas at Austin (US)
Lockheed Martin
Openalex Percentile: Top 40%
Control Systems and Identification
0.33
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Direct Multi‐Thread Adaptive Control With Attracting Manifold Design — Maruthi Ram Akella, Richard D. Hoobler · International Journal of Adaptive Control and Signal Processing (2024) | TGRS Research Map | TGRS