The Research on Height Control of Airship with Constant Flying Speed

Xin Li Zhang; Yun An Hu; Di Liu

doi:10.4028/www.scientific.net/AMM.644-650.875

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HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vols. 644-650The Research on Height Control of Airship with...

The Research on Height Control of Airship with Constant Flying Speed

Abstract:

The PID control scheme of airship with fixed flying high is studied in allusion to pitch channel nonlinear model of a class of stratosphere airship in this paper. The traditional PID control law is designed aim at the fixed high flight control of airship. The detailed simulation analysis is presented. It indicates that the airship can realize the fixed high flight in the range of 1000 meters. When flying high increase further, PID control scheme is not reasonable because instruction is too large. At the same time, the speed of engine has large influence on PID control scheme. The research of paper has good technical reference value for design and experiments of stratosphere airship.

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Periodical:

Applied Mechanics and Materials (Volumes 644-650)

Pages:

875-878

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.644-650.875

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Cite this paper

Online since:

September 2014

Authors:

Xin Li Zhang*, Yun An Hu, Di Liu

Keywords:

Airship, Constant Speed, Noise, PID Control, Pitching Angle

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* - Corresponding Author

References

[1] De Paiva E C, Bueno S S, Bergerman M. A Robust Pitch Attitude Controller for AURORA's Semi-Autonomous Robotic Airship[J]. American Institute of Aeronautics & Astronautics. 1999. AIAA-99-3907, 141-148.

DOI: 10.2514/6.1999-3907

Google Scholar

[2] Silveira G F, Garvalho J R H, Madrid M K, et al. Lateral Control of An Aerial Unmanned Robot Using Visual Servoing Techniques[J]. The 2nd Workshop on Robot Motion and Control, 2001, 263-268.

DOI: 10.1109/romoco.2001.973465

Google Scholar

[3] Azinheira, J.R., A. Moutinho, Hover Control of an UAV With Backstepping Design Including Input Saturations[J]. IEEE Transactions on Control System Technology, 2008. 16(3): 517-526.

DOI: 10.1109/tcst.2007.908209

Google Scholar

[4] Azinheira J R, Moutinho A, Paiva E C. A backstepping controller for path-tracking of an underactuated autonomous aitship. [J] International Journal of Robust and Nonlinear Control, 2009, 19(4): 418-441.

DOI: 10.1002/rnc.1325

Google Scholar

[5] Repoulias F, Papadopoulos E. Robotic airship trajectory tracking control using a backstepping methodology. [C] In: 2008 IEEE International Conference on Robotics and Automation, Pasadena, CA, USA, (2008).

DOI: 10.1109/robot.2008.4543207

Google Scholar

[6] Sergio B. Varella Gomes, Josue Jr.G. Ramos. Airship dynamic modeling for autonomous operation[C]. Proceedings of the 2003 IEEE. International Conference on Robotics & Automation. 2003: 5~14.

DOI: 10.1109/robot.1998.680973

Google Scholar

[7] Joseph B. Mueller, Michael A. Paluszek, Yiyuan Zhao. Development of an Aerodynamic Model and Control Law Design for a High Altitude Airship[C]. AIAA 3rd Unmanned Unlimited, Technical Conference, Workshop and Exhibit, Chicago, Illinois, 2004: 2~17.

DOI: 10.2514/6.2004-6479

Google Scholar