Study of a Four Rotor Aircraft Modeling

Yang Jin Xian; Li Zhi Peng; Chen Chao

doi:10.4028/www.scientific.net/AMM.494-495.293

Paper Titles

Finite Element Analysis of Material Mechanics Experiment
p.277

Design and Implementation of the Disassembly and Assembly Equipment to the Buffer Braking Device of the Elevating Mechanism of the Heavy Caliber Ground Artillery
p.281

The Experimental Study on the Enhanced Evaporating Property of the Pineapple Juice by Ultrasound
p.285

Research on Temperature Distribution and Stress Distribution Model of Prefabricate Block Electric Furnace Roof
p.289

Study of a Four Rotor Aircraft Modeling
p.293

Preliminary Exploration of the Dynamic Model and Experiment on an Impact between a Tennis Ball and Racket
p.297

Sports Biomechanical Research and Exploration on the Tennis Injuries
p.301

RETRACTED: Structure Optimization of Agricultural Vehicle Frame Based on APDL
p.305

Analysis of Air-Flow Field of Large Ships in Waves
p.309

HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vols. 494-495Study of a Four Rotor Aircraft Modeling

Study of a Four Rotor Aircraft Modeling

Abstract:

In order to design the four rotor aircraft attitude control system, take the hover state or low speed flight state as a benchmark, firstly, divide the aircraft model into linear motion model and the angular motion model and model it separately, the nonlinear mathematical model of aircraft can be obtained. And then use the small disturbance linearization principle to linear mathematical model for a simplified model. After substituting into the previous experimental data, the mathematical model which controller design needs is got.

You might also be interested in these eBooks

Current Development of Mechanical Engineering and Energy

View Preview

Info:

Periodical:

Applied Mechanics and Materials (Volumes 494-495)

Pages:

293-296

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.494-495.293

Citation:

Cite this paper

Online since:

February 2014

Authors:

Yang Jin Xian*, Li Zhi Peng, Chen Chao

Keywords:

Analysis, Four Rotor Aircraft, Modeling

Export:

RIS, BibTeX

Price:

Permissions:

Request Permissions

* - Corresponding Author

References

[1] Wang Junsheng, Ma Hongxu Cai Wenlan, tax waves, NieBoWen. Method of unmanned helicopter control small four rotor based on ADRC [J]. Journal of Projectiles Rockets Missiles and Guidance. 2008 (3) : 31 to 40.

Google Scholar

[2] Hu Yuqun. Study on some dynamic problems of micro air vehicle[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, (2002).

Google Scholar

[3] HongSenTao Jin Zhihui, li chi keung. Four rotor aircraft modeling and postural stability analysis [J]. Electronic and Electro-optical Systems 2006 (5) : 91-94.

Google Scholar

[4] J. F. GUERRERO CASTELLANOS, A. HABLY, N. MARCHAND, S. LESECQ. Bounded attitude stabilization: Application on four-rotor helicopter[J]. 2007 IEEE Intemational Conference on Robotics and Automation. 2007: 730-735.

DOI: 10.1109/robot.2007.363073

Google Scholar

[5] L. Derafa, T. MADani, A. Benallegue. Dynamic Modelling and Experimental Identification of Four Rotors Helicopter Permanents[J]. IEEE Intematonal conference on Industrial Technology. 2006: 1834-1839.

DOI: 10.1109/icit.2006.372515

Google Scholar