Highly Scalable Flight Control Architecture for Small Autonomous Helicopter Using PC104/ARM Technology

Shu Xun Zhou; Jie An; Jian Guo Yao; Fei Hu

doi:10.4028/www.scientific.net/AMR.748.718

Paper Titles

Study on Design Proposal of Computerized Numerical Control Machine Networking
p.699

A Linear Camera Calibration Applying in Servo Mechanical Arm System with One Camera
p.704

Sound Analysis and Synthesis for Audio Simulation System of Flight Simulator
p.708

Research on the Vision Processing of Space Robot's Tracking Camera
p.713

Highly Scalable Flight Control Architecture for Small Autonomous Helicopter Using PC104/ARM Technology
p.718

The Design of Servo System for Azimuth of Directional Antenna Based on PMSM
p.723

Unmanned Helicopter Course PID Controller Parameters Setting and Simulation
p.727

Application of Sliding Mode Cascade Controller in AC Servo System
p.731

Modal Analysis of Permanent Magnet Synchronous Motor of Electric Vehicles
p.735

HomeAdvanced Materials ResearchAdvanced Materials Research Vol. 748Highly Scalable Flight Control Architecture for...

Highly Scalable Flight Control Architecture for Small Autonomous Helicopter Using PC104/ARM Technology

Abstract:

Autonomous helicopter flight presents challenges in flight control system design with scalability. In this paper, we present the integration architecture of hardware and software for the flight control system based TREX 600 helicopter. In order to enhance scalability, the flight control system uses the PC104 and the ARM which is exerted to process the measurement data, including the position, attitude, height etc. The flight control is developed based multi-loop decoupling PID control which is easy to be implemented. Finally, the flight control system is successfully verified in the actual autonomous flight control experiment.

You might also be interested in these eBooks

Material and Manufacturing Technology IV

View Preview

Info:

Periodical:

Advanced Materials Research (Volume 748)

Pages:

718-722

DOI:

https://doi.org/10.4028/www.scientific.net/AMR.748.718

Citation:

Cite this paper

Online since:

August 2013

Authors:

Shu Xun Zhou, Jie An, Jian Guo Yao, Fei Hu

Keywords:

Flight Control, PC104/ARM, PID, Scalable

Export:

RIS, BibTeX

Price:

Permissions CCC:

Request Permissions

Permissions PLS:

Request Permissions

Сopyright:

Citation:

References

[1] Juntong Qi, Dalei Song, Lei Dai and Jianda Han, The ServoHeli-20 Rotorcraft UAV Project, 15th International conference on Mechatronics and Machine Vision in Practice(M2VIP08), Auckland, New-Zealand, December (2008).

DOI: 10.1109/mmvip.2008.4749513

Google Scholar

[2] Guowei Cai, Ben M. CHEN and Tong H. LEE, An overview on development of miniature unmanned rotorcraft systems, Frontiers of Electrical and Electronic Engineering in China, Vol. 5, (1), pp.1-14, China, (2010).

DOI: 10.1007/s11460-009-0065-3

Google Scholar

[3] Dongdong Liu and Hailong Pei, Unmanned helicopter hardware system design based on ARM7, , Computer engineering and design, Vol. 30, (6), p.1394, (2009).

Google Scholar

[4] Weifeng Cai, Hailong Pei, Autonomous unmanned helicopter software design based on ARM, , Fujian Computer, Vol. 12, April (2008).

Google Scholar

[5] Yu Gu, Brad Seanor, Srikanth Gururajan and Marcello R. Napolitano Integrated Avionics System for Research UAVs, (2008).

DOI: 10.2514/6.2008-7490

Google Scholar

[6] Xin Su, Yanhui Wan and Bo Xie, Sigle antenna DGPS directional attitude measurement method research based on the tracking differentiator, Missiles and Guidance Journal, Vol. 31, April (2011).

Google Scholar

[7] Jingqing Han and Lulin Yuan, The discrete form of tracking differentiator, Journal of systems science and Mathematical Sciences, Vol. 19, (3), pp.268-273, July (1999).

Google Scholar

[8] Davic Hyunchul Shim, Hyoun Jin Kim, and Shankar Sastry, HIERARCHICAL CONTROL SYSTEM SYNTHESIS FOR ROTROCRAFT-BASED UNMANNED AERIAL VEHICLES, AIAA Guidance, Navigation and Control Conference, A00-37046, Denver, August (2000).

DOI: 10.2514/6.2000-4057

Google Scholar