Tai et al., 2023 - Google Patents
Research on Dynamic Characteristics Analysis and Control Law Design Method of Model Aircraft in Wind Tunnel–Based Virtual Flight TestingTai et al., 2023
View PDF- Document ID
- 11113772540248148549
- Author
- Tai S
- Wang L
- Wang Y
- Bu C
- Yue T
- Liu H
- Publication year
- Publication venue
- Journal of Aerospace Engineering
External Links
Snippet
In the three-degree-of-freedom virtual flight test, the scaled model has no translational motion, which will result in the model's dynamics being different from that of free flight, and this difference will directly affect its effectiveness in simulating free flight and the design of …
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
-
- 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
- G05D1/04—Control of altitude or depth
- G05D1/042—Control of altitude or depth specially adapted for aircraft
- G05D1/046—Control of altitude or depth specially adapted for aircraft to counteract a perturbation, e.g. gust of wind
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