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15 - General Engineering

University of Leicester

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Output 69 of 99 in the submission

Article title

Pilot-Involved-Oscillation Suppression Using Low-Order Antiwindup: Flight-Test Evaluation

Type

D - Journal article

DOI

10.2514/1.54441

Title of journal

JOURNAL OF GUIDANCE CONTROL AND DYNAMICS

Article number

Volume number

Issue number

First page of article

471

ISSN of journal

0731-5090

Year of publication

2012

URL

Number of additional authors

Additional information

This paper reports flight test results from several campaigns carried out by Leicester in conjunction with Deimos Space (Technical Lead, Dr. Murray Kerr - murray.kerr@deimos-space.com) and DLR (German Aerospace Center). This paper describes how the addition of anti-windup compensation can greatly reduce the tendency of an agile aircraft so suffer from so-called pilot-induced-oscillations (PIO's). This work has also generated several conference publications and MCT was awarded "Best Presentation" for an invited talk at the US Guidance and Systems Committee meeting in September 2008. This work was partially responsible for award of the £178K MoD/DGA "Dynamic Controllers" project to Leicester.

Interdisciplinary

Cross-referral requested

Research group

B - Control Systems

Proposed double-weighted

Double-weighted statement

Reserve for a double-weighted output

Non-English

English abstract