Tantaroudas et al., 2015 - Google Patents
Model order reduction for control design of flexible free-flying aircraftTantaroudas et al., 2015
View PDF- 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 …
- 230000001603 reducing 0 title abstract description 19
Classifications
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- 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
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- 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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