Design of Four-Rotor Unmanned Aircraft Control System Based on ARM

Chang Zhi Lv; Yun Can Hao; Di Fan; Lu Wan

doi:10.4028/www.scientific.net/AMM.711.324

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HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vol. 711Design of Four-Rotor Unmanned Aircraft Control...

Design of Four-Rotor Unmanned Aircraft Control System Based on ARM

Abstract:

As a new type of vertical take-off and landing unmanned aerial vehicles, four-rotor unmanned aircraft has strong load capacity, simple structure, flexible operation Characteristics, so it is the preferred method of execution the air, and is widely used in military and civil field. Based on four-rotor aircraft structure and movement theory, this paper designs the aircaft control system based on ARM. Based on upper machine, the design of PID control algorithm was tested in this paper. From the results, the stability of the controller is good, and its speed control is superior to the single closed-loop.

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Periodical:

Applied Mechanics and Materials (Volume 711)

Pages:

324-328

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.711.324

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Online since:

December 2014

Authors:

Chang Zhi Lv, Yun Can Hao*, Di Fan, Lu Wan

Keywords:

Attitude, Four-Rotor Aircraft, Heading Angle, PID Double-Loop Control, Pitch, Roll

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* - Corresponding Author

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