FLIGHT CONTROL USING ADAPTIVE DYNAMIC INVERSION

Q: How can I download an article?

To download an article from SID, first log in to the site, search for the article title, and click on the 'Download Article' option.

Q: How can I download an ISI article?

To download an ISI article on SID, enter the keyword or article title in the search bar, view the relevant results, click on the desired article, and select the 'Download Article' option.

Q: How can I access the SID database?

To access the SID database, visit SID.ir, create an account, and log in to access scientific resources.

Q: Is downloading articles from SID free?

Some articles on SID are available for free, while others require payment. Details are specified on the article's page.

MOBINI BIDGOLI MARYAM; SADATI SEYED HOSSEIN

مرکز اطلاعات علمی Scientific Information Database (SID) - Trusted Source for Research and Academic Resources

Journal Paper

Paper Information

Journal: AEROSPACE KNOWLEDGE AND TECHNOLOGY JOURNAL Year:2016 | Volume:5 | Issue:1 Page(s): 7-16

Download Full-Text

Persian Verion

View:

1,114

Download:

Cites:

Information Journal Paper

Title

FLIGHT CONTROL USING ADAPTIVE DYNAMIC INVERSION

Author(s)

MOBINI BIDGOLI MARYAM | SADATI SEYED HOSSEIN | Issue Writer Certificate

Keywords

FLIGHT CONTROLLERQ1

ADAPTIVE DYNAMICS INVERSIONQ1

DYNAMICS INVERSIONQ2

ADAPTIVE CONTROLLERQ1

TIME-SCALE SEPARATIONQ1

Abstract

This paper discusses the ﬂight control strategy based on Adaptive Dynamic Inversion (ADI) with two-time-scale separation for airplane. Because of nonlinear behavior of flight dynamics, the flight control problem is a rather important and complex issue. In addition to traditional methods, e.g., classic controller, Dynamic inversion methods, fuzzy and neural networks have been used. After reviewing these methods, Combination Adaptive dynamic inversion Method is designed. In this structure, the control system attempts to track the angle of attack, the sideslip angle and the roll angle in wind frame (m, a, b). Six degree-of-freedom nonlinear equations of motion are considered for tracking the input commands. Dynamic inversion technique needs an exact and accurate flight dynamics, and to avoid this problem, we use an ADAPTIVE CONTROLLER. Two-timescale based system dynamics are divided into slow outer variables and fast inner variables. ADAPTIVE CONTROLLER and Dynamic inversion algorithm are used in inner and outer loops, respectively. The performance of the proposed method compares with Full Dynamic Inversion (DI) method. Simulation results demonstrated the efficacy of Adaptive Dynamic Inversion controller.

Cites

No record.

References

No record.

Cite

APA: Copy

MOBINI BIDGOLI, MARYAM, & SADATI, SEYED HOSSEIN. (2016). FLIGHT CONTROL USING ADAPTIVE DYNAMIC INVERSION. AEROSPACE KNOWLEDGE AND TECHNOLOGY JOURNAL, 5(1 ), 7-16. SID. https://sid.ir/paper/264182/en

Vancouver: Copy

MOBINI BIDGOLI MARYAM, SADATI SEYED HOSSEIN. FLIGHT CONTROL USING ADAPTIVE DYNAMIC INVERSION. AEROSPACE KNOWLEDGE AND TECHNOLOGY JOURNAL[Internet]. 2016;5(1 ):7-16. Available from: https://sid.ir/paper/264182/en

IEEE: Copy

MARYAM MOBINI BIDGOLI, and SEYED HOSSEIN SADATI, “FLIGHT CONTROL USING ADAPTIVE DYNAMIC INVERSION,” AEROSPACE KNOWLEDGE AND TECHNOLOGY JOURNAL, vol. 5, no. 1 , pp. 7–16, 2016, [Online]. Available: https://sid.ir/paper/264182/en

Related Journal Papers