Attitude Control of Aircraft Using Only Synthetic Jet Actuators When Stall Occurs Article Swipe
Chunzhi Li
,
Tingting Zhang
,
Jianying Yang
·
YOU?
·
· 2018
· Open Access
·
· DOI: https://doi.org/10.1109/access.2018.2853145
YOU?
·
· 2018
· Open Access
·
· DOI: https://doi.org/10.1109/access.2018.2853145
This paper proposes a novel active flow control method for a special aircraft, that using only synthetic jet actuators (SJAs) to achieve pitch-roll-yaw attitude control at a high angle of attack when the stall occurs. The special aircraft goes without traditional aileron, elevator, or vertical stabilizer. As the first step, the model of the aircraft is built and the relation between the velocity amplitude of SJAs and the moments provided by SJAs are derived. The next step, to solve the problem that parameter uncertainties, unmodeled dynamics, and unknown external disturbances exist in the aircraft system, a sliding mode controller base on extended state observer (ESO) is designed. The parameter uncertainties, unmodeled dynamics, and unknown external disturbances are regarded as the compound interference of the system, which is estimated by the ESO and compensated in real time. Finally, the effectiveness of the proposed controller is verified through the numerical simulations. Simulation results show that the proposed control method is feasible and effective to solve the difficult problem of attitude control when the stall occurs.
Related Topics
Concepts
Aileron
Control theory (sociology)
Stall (fluid mechanics)
Actuator
Elevator
Computer science
Flight control surfaces
Attitude control
Control system
Angle of attack
Aerodynamics
Engineering
Control engineering
Control (management)
Aerospace engineering
Artificial intelligence
Electrical engineering
Metadata
- Type
- article
- Language
- en
- Landing Page
- https://doi.org/10.1109/access.2018.2853145
- OA Status
- gold
- Cited By
- 9
- References
- 30
- Related Works
- 10
- OpenAlex ID
- https://openalex.org/W2863109823
All OpenAlex metadata
Raw OpenAlex JSON
- OpenAlex ID
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https://openalex.org/W2863109823Canonical identifier for this work in OpenAlex
- DOI
-
https://doi.org/10.1109/access.2018.2853145Digital Object Identifier
- Title
-
Attitude Control of Aircraft Using Only Synthetic Jet Actuators When Stall OccursWork title
- Type
-
articleOpenAlex work type
- Language
-
enPrimary language
- Publication year
-
2018Year of publication
- Publication date
-
2018-01-01Full publication date if available
- Authors
-
Chunzhi Li, Tingting Zhang, Jianying YangList of authors in order
- Landing page
-
https://doi.org/10.1109/access.2018.2853145Publisher landing page
- Open access
-
YesWhether a free full text is available
- OA status
-
goldOpen access status per OpenAlex
- OA URL
-
https://doi.org/10.1109/access.2018.2853145Direct OA link when available
- Concepts
-
Aileron, Control theory (sociology), Stall (fluid mechanics), Actuator, Elevator, Computer science, Flight control surfaces, Attitude control, Control system, Angle of attack, Aerodynamics, Engineering, Control engineering, Control (management), Aerospace engineering, Artificial intelligence, Electrical engineeringTop concepts (fields/topics) attached by OpenAlex
- Cited by
-
9Total citation count in OpenAlex
- Citations by year (recent)
-
2023: 2, 2022: 3, 2021: 2, 2019: 2Per-year citation counts (last 5 years)
- References (count)
-
30Number of works referenced by this work
- Related works (count)
-
10Other works algorithmically related by OpenAlex
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| referenced_works | https://openalex.org/W2317492854, https://openalex.org/W3175615486, https://openalex.org/W2095544020, https://openalex.org/W1976802301, https://openalex.org/W2071374733, https://openalex.org/W2018512092, https://openalex.org/W1520875462, https://openalex.org/W2413188661, https://openalex.org/W2130672516, https://openalex.org/W2070478661, https://openalex.org/W6742055562, https://openalex.org/W2157540237, https://openalex.org/W2158826490, https://openalex.org/W4236960545, https://openalex.org/W2256560093, https://openalex.org/W2102911857, https://openalex.org/W2318006633, https://openalex.org/W6685274010, https://openalex.org/W2332154246, https://openalex.org/W1972386460, https://openalex.org/W2135493101, https://openalex.org/W2161798039, https://openalex.org/W1982923176, https://openalex.org/W1989421683, https://openalex.org/W2160729924, https://openalex.org/W2053892268, https://openalex.org/W2509245172, https://openalex.org/W2737787629, https://openalex.org/W2170113567, https://openalex.org/W2071794179 |
| referenced_works_count | 30 |
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