The Analysis of Multi-Rotor Attitude Simulator Based on Matlab

Abstract:

There exist overfrequency issues of airframe vibration, instable fight conditions, inefficient airframe survivability and undeveloped cockpit’s eject-ability insides multi-rotor aircraft flights. This paper focuses on four-rotor aircraft researches via gathering inherent rotor attitudes with the inertial motion capture device. Based-on the resulting data analyses, the relations between flight attitudes and rotor performances are clearly figured out. This research also advances multi-rotor aircraft works, such as: drawing frameworks, evaluating simulations, designing control systems, and optimizing safety and stability properties.

• Periodical: Applied Mechanics and Materials (Volumes 670-671)
• Pages: 1350-1357
• DOI: https://doi.org/10.4028/www.scientific.net/AMM.670-671.1350
• Online since: October 2014
• Authors: Zheng Xu Zhao, Li Long Han*, Qian Xu
• Keywords: Attitude Analysis, Inertial Motion Capture, Multi-Rotor Aircraft

References

[1] Jiaqi Zhang, Research on the Attitude Motion Control of Quadrotor, Northeastern University, Northeastern University , Shenyang, China, (2009). In Chinese.

[2] Chunjun Wu, Binghong Zhou, Wireless Attitude Measurement System Based on MEMS, Instrument Technique and Sensor, Instrument Technique and Sensor, Shenyang, Liaoning, China, No. 8 (2013), pp.76-78. In Chinese.

[3] Xiaojie Liu, Study and Implementation of Position and Attitude Estimation for Four-rotor Mini Rotorcraft Based on Vision, Jilin University, Jilin University, Changchun, China, (2009). In Chinese.

[4] Nicom Promkajin, Manukid Parnichkun, Attitude and altitude control of a four-rotor hovercraft using sliding mode control with adaptive sliding surface, 2011 IEEE International Conference on Robotics and Biomimetics, IEEE Computer Society, Shanghai, China, (2011).

DOI: 10.1109/robio.2011.6181465

[5] Caizheng Xu, Ting Zhang, The optimal attitude controller design and simulation of three-axis dual rotor helicopter, Applied Mechanics and Materials, Trans Tech Publications, Sanya, China, 2012, 128-129, pp.1265-1268. In Chinese.

DOI: 10.4028/www.scientific.net/amm.128-129.1265

[6] Iván González, Sergio Salazar, Jorge Torres, Rogelio Lozano, Hugo Romero, Real-time attitude stabilization of a mini-UAV quad-rotor using motor speed feedback, Journal of Intelligent and Robotic Systems, Theory and Applications, Springer Netherlands, Vol. 70 (2013).

DOI: 10.1007/s10846-012-9713-6

[7] Jeong Seungho, Jung Seul, Design and experimental studies of a disturbance observer for attitude control of a quad-rotor system, Journal of Institute of Control, Robotics and Systems, Institute of Control, Robotics and Systems, Vol. 19(2013).

DOI: 10.5302/j.icros.2013.13.1890

[8] Raimúndez Cesáreo, Camaño José Luis, Tracking in scale quad-rotors through adaptive augmentation, Neural Computign & Application, Springer London, Vol. 23 (2013), No. 3-4, pp.635-643.

DOI: 10.1007/s00521-013-1425-8

[9] Lilong Han, Zhengxu Zhao, Research of Multi-Rotor Attitude Posture based on Inertial Motion Capture, Journal of the Hebei Academy of Sciences, the Hebei Academy of Sciences, Shijiazhuang, Hebei, China, Vol. 30 (2013), NO. 2, pp.1-6. In Chinese.

DOI: 10.17660/ejhs.2019/84.6.3

[10] Zhengxu Zhao, Huan Dai, Zhao Wenbin, Yuan Jie, Human Motion Posture Simulation Based on Inertial Motion Capture, Computer Engineering, Computer Engineering, Shanghai, China, Vol. 38 (2012), No. 5, pp.5-8. In Chinese.

[11] Zhijun Liu, Qiang Lv, Wang Donglai, Modeling And Simulation Control Of a Small – sized Quadrotor Helicopter, Computer Simulation, Computer Simulation, Beijing, China, Vol. 27 (2010), No. 7, pp.18-20. In Chinese.