You are in : Home » Results & submissions » Select UOA » 15 - General Engineering » View submission: University of Bristol » Outputs » Detail

Output details

15 - General Engineering

University of Bristol

Return to search Previous output Next output

Output 0 of 0 in the submission

Article title

Analysis of Conventional and Asymmetric Aircraft Configurations Using CEASIOM

Type

D - Journal article

DOI

10.1016/j.paerosci.2011.08.008

Title of journal

Progress in Aerospace Sciences

Article number

Volume number

Issue number

First page of article

647

ISSN of journal

03760421

Year of publication

2011

URL

http://www.sciencedirect.com/science/article/pii/S0376042111000741

Number of additional authors

Additional information

Paper presents asymmetric aircraft that offers potential for drag reduction and therefore improved efficiency. However, this results in highly-unstable configuration which has coupled response to any control input. Paper demonstrated successful application of Eigenstructure assigment to decouple the open-loop asymmetric-aircraft response. Closed-loop response is presented with performance analysis in order to highlight performance benefits. Work was presented in invited session at 2010 AIAA Atmospheric Flight Mechanics Conference (Toronto, Canada).

Interdisciplinary

Cross-referral requested

Research group

I - Robotics

Proposed double-weighted

Double-weighted statement

Reserve for a double-weighted output

Non-English

English abstract