Design of Quadrotor’s Control System Based on DSP

Qiang Lv; Pei Pei Ni; Guo Sheng Wang; Feng Liu

doi:10.4028/www.scientific.net/AMR.989-994.3216

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HomeAdvanced Materials ResearchAdvanced Materials Research Vols. 989-994Design of Quadrotor’s Control System Based on DSP

Design of Quadrotor’s Control System Based on DSP

Abstract:

A problem of quadrotor’s control system based on DSP is investigated in this paper. STMS320F28335 is used as the main processer, due to its advantages of high-speed processing capability and powerful floating point processing capability. The inertial measurement unit is selected for inner-loop attitude control, while the optical flow sensor is adopted for outer-loop attitude compensation. Infrared range finder is choosed for altitude control with PID method. Quadrotor uses XBee-Pro wireless module to contact with ground station and sends statement information in accordance with the Mavlink protocol. Test results show that the control system is reliable and can meet the requirement of the attitude control system.

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Periodical:

Advanced Materials Research (Volumes 989-994)

Pages:

3216-3219

DOI:

https://doi.org/10.4028/www.scientific.net/AMR.989-994.3216

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Online since:

July 2014

Authors:

Qiang Lv*, Pei Pei Ni, Guo Sheng Wang, Feng Liu

Keywords:

Attitude Control, DSP, Inertial Measurement Unit (IMU), Optical Flow Sensor, Quadrotor

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References

[1] Q Lv, D L Wang, F Liu and H R Bai: Discrete-time Mode Variable Structure Control Based on Nonlinear Exponential Reaching Law. Journal of Projectiles, Rockets, Missiles and Guidance. Vol. 32, No. 5 (2012), p: 50-54: 25-28.

Google Scholar

[2] F Guo. Localization for Quadrotor Unmaned Aerial Vehicle in Complex Environment . Master thesis. Tianjin: Tianjin University, (2012).

Google Scholar

[3] M Ji, J T Lu. Design of quadcopter's control system based on Cortex-M4. Computer & Control, Vol. 21, No. 7 (2013), p: 1816-1821.

Google Scholar

[4] L Wang. Research on control technology of quadrotor unmanned aerial vehicle. Master thesis. Harbin: Harbin Engineering University, (2012).

Google Scholar