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Tantaroudas et al., 2015 - Google Patents

Model order reduction for control design of flexible free-flying aircraft

Tantaroudas et al., 2015

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Document ID
6174824958358585182
Author
Tantaroudas N
Da Ronch A
Badcock K
Wang Y
Palacios R
Publication year
Publication venue
AIAA Atmospheric Flight Mechanics Conference

External Links

Snippet

The NASA Helios flight accident in 2003 triggered an increased interest the fluid-structure coupling that occurs in light, very flexible and high aspect ratio wings. 1 The usual separation of flight dynamics and linear aeroelastic analysis is not appropriate for gust …
Continue reading at eprints.soton.ac.uk (PDF) (other versions)

Classifications

    • G—PHYSICS
    • G06—COMPUTING; CALCULATING; COUNTING
    • G06F—ELECTRICAL DIGITAL DATA PROCESSING
    • G06F17/00—Digital computing or data processing equipment or methods, specially adapted for specific functions
    • G06F17/50—Computer-aided design
    • G06F17/5009—Computer-aided design using simulation
    • G06F17/5018—Computer-aided design using simulation using finite difference methods or finite element methods
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
    • G05D1/08—Control of attitude, i.e. control of roll, pitch, or yaw
    • G05D1/0808—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft
    • G05D1/0816—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft to ensure stability
    • G05D1/0825—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft to ensure stability using mathematical models

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