Gryte et al., 2018 - Google Patents
Aerodynamic modeling of the skywalker x8 fixed-wing unmanned aerial vehicleGryte et al., 2018
View PDF- Document ID
- 9659697215123957123
- Author
- Gryte K
- Hann R
- Alam M
- Roháč J
- Johansen T
- Fossen T
- Publication year
- Publication venue
- 2018 International Conference on Unmanned Aircraft Systems (ICUAS)
External Links
Snippet
With advanced control, estimation and simulation requirements in unmanned aerial systems comes the need for sophisticated aerodynamic models. This paper reviews two common means for establishing such models; numerical design tools and wind tunnel testing, by …
- 238000004088 simulation 0 abstract description 4
Classifications
-
- 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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