Autopilot Design Using Nonlinear Control and PIL Test for Landing a UAV

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Ghesmati A.; Hossein Sadati S.; Ghesmati A.; ABBASI Y.

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Journal Paper

Paper Information

Journal: JOURNAL OF MECHANICAL ENGINEERING Year:2019 | Volume:49 | Issue:1 (86) Page(s): 219-228

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Information Journal Paper

Title

Autopilot Design Using Nonlinear Control and PIL Test for Landing a UAV

Author(s)

Ghesmati A. | Hossein Sadati S. | Ghesmati A. | ABBASI Y. | Issue Writer Certificate

Keywords

Auto Landing

Flare

Nonlinear Dynamics Inversion

Autopilot

Real time

Abstract

Undoubtedly, the flight control system is one of the most important parts of an aeronautical vehicles that has duty of stability and achieve good performance in execution of commands. In flight control according to nonlinear dynamics, time varying and structural and parametric uncertainties of aeronautical vehicles, various control approaches use to achieve stability, good performance and reduce the effect of the uncertainties and modeling error. In this paper, Autopilot software design were developed using Nonlinear Dynamics Inversion controller to landing a UAV in two stages. Also, with using DSP hardware and CPU TMS320F28335, Nonlinear Dynamics Inversion Autopilot software were implemented and tested to Real time PIL stage. Finally, nonlinear six-degree-of-freedom simulation results at real-time, confirm proper performance of implementation.

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APA: Copy

Ghesmati, A., Hossein Sadati, S., Ghesmati, A., & ABBASI, Y.. (2019). Autopilot Design Using Nonlinear Control and PIL Test for Landing a UAV. JOURNAL OF MECHANICAL ENGINEERING, 49(1 (86) ), 219-228. SID. https://sid.ir/paper/269949/en

Vancouver: Copy

Ghesmati A., Hossein Sadati S., Ghesmati A., ABBASI Y.. Autopilot Design Using Nonlinear Control and PIL Test for Landing a UAV. JOURNAL OF MECHANICAL ENGINEERING[Internet]. 2019;49(1 (86) ):219-228. Available from: https://sid.ir/paper/269949/en

IEEE: Copy

A. Ghesmati, S. Hossein Sadati, A. Ghesmati, and Y. ABBASI, “Autopilot Design Using Nonlinear Control and PIL Test for Landing a UAV,” JOURNAL OF MECHANICAL ENGINEERING, vol. 49, no. 1 (86) , pp. 219–228, 2019, [Online]. Available: https://sid.ir/paper/269949/en

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