Computation of Controllability Regions for Unstable Aircraft Dynamics

descriptionPublicationkeyboard_double_arrow_right Article 01 Jul 2004 United Kingdom English Publisher:American Institute of Aeronautics and Astronautics (AIAA)Journal:Journal of Guidance, Control, and Dynamics, volume 27, pages 647-656 (issn: 0731-5090, eissn: 1533-3884,

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Authors: Goman, M. (Mikhail G.); Demenkov, M. N. (Max);

doi: 10.2514/1.4038

handle: 2086/316

Computation of Controllability Regions for Unstable Aircraft Dynamics

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Abstract

This output describes an approach based on geometrical and optimisation principles that resulted in efficient software tools for computation of null controllability region of unstable dynamical systems. The software toolset, “Stabcalcs” has been created and tested on several flight dynamics applications and delivered to DERA/QinetiQ Ltd. within Computational Framework for flight clearance applications (in 2002-2003, DERA/QinetiQ Ltd Technical Manager Yoge Patel, yoge@bbsr.co.uk). The research was sponsored by QinetiQ Ltd.

Country

United Kingdom

Related Organizations

De Montfort University
United Kingdom

Keywords

RAE 2008, UoA 28 Mechanical, Aeronautical and Manufacturing Engineering

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