Design of Flight Control System Bus Controller of UAV Based on Double CAN-Bus

Ji Hui Pan; Sheng Bing Zhang; Hao Ma

doi:10.4028/www.scientific.net/AMM.479-480.641

Paper Titles

Whole-Body Human-to-Humanoid Motion Imitation
p.617

The Development of a Hybrid Antilock Braking System Using Magnetorheological Brake
p.622

Optimization of the Neural Muscular Drive and Respiratory Signals under Dead Space Loading and CO₂ Inhalation
p.627

Development of an Automatic Optical Inspection System and its Application to Defect Examination
p.636

Design of Flight Control System Bus Controller of UAV Based on Double CAN-Bus
p.641

A Wireless Sensor Network Deployment Planning Tool to Support Building Automation
p.646

Cryptanalysis and Improvement of Secure Key Distribution for the Smart Grid
p.651

Study and Design of Smart Embedded Home System Based on Wireless Electric Power Measurement Monitoring System
p.656

Home Security Service and Condition Control
p.661

HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vols. 479-480Design of Flight Control System Bus Controller of...

Design of Flight Control System Bus Controller of UAV Based on Double CAN-Bus

Abstract:

This paper represents a new interconnected architecture of Flight control System (FCS). It can solve the problems of massive equipment and large cross link information. The interconnected architecture adopts double CAN-Bus to construct a redundant flight control systematic bus. This paper will illustrate the characters of double CAN-Bus comparing with the characters of CAN-Bus firstly. Then it will present the bus controller hardware design, allowance design, network communication protocol, software flow and code design respectively. The experimental results show that the bus is running well, can satisfy the small vehicle control system of a high real time capability and node demand, at the same time system has high reliability, open etc.

You might also be interested in these eBooks

Applied Science and Precision Engineering Innovation

View Preview

Info:

Periodical:

Applied Mechanics and Materials (Volumes 479-480)

Pages:

641-645

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.479-480.641

Citation:

Cite this paper

Online since:

December 2013

Authors:

Ji Hui Pan, Sheng Bing Zhang, Hao Ma

Keywords:

Double CAN Bus, FCS, Small Aircraft

Export:

RIS, BibTeX

Price:

Permissions CCC:

Request Permissions

Permissions PLS:

Request Permissions

Сopyright:

Citation:

References

[1] Unmanned Systems Roadmap 2007-2032 [R]. U. S. Office of the Secretary of Defense 2007. chapter 1.

Google Scholar

[2] Michael Stock flight system, CAN aerospace interface specification for airborne CAN applications V1. 7[R/OL], 2010, chapter 2.

Google Scholar

[3] Liu G.Z., Lin.H., Li,Y., Design of dual-redundancy Actuator Control System, Micro Motos. 1（43) 71–75 (2010).

Google Scholar

[4] Zhang.L., Zhu.M., Wu.Z., CAN bus application layer protocol design for an unmanned helicopter system, Journal of Beijing University of Aeronautics and Astronautics. 10, 37 (2011).

Google Scholar

[5] W. Wang, H. Taylor, Z. Reg. Extended state observer-based robust fault-tolerant controller for flight control surface failures. Proc. Of 9th International Conference on Electronic Measurement & Instruments, 2009: 610–615.

DOI: 10.1109/icemi.2009.5274219

Google Scholar

[6] Pan Jihui. Design of Double CANBus communication system for small aircraft. Computer measurement and control. 18( 1): 78-81 2010 [in Chinese].

Google Scholar