NDLI: Hardware-in-the-loop development system for rotary-wing/fixed-wing UAVs

Content Provider	IEEE Xplore Digital Library
Author	Juntong Qi Jinda Liu
Copyright Year	2013
Description	Author affiliation: Coll. of Inf. Sci. & Eng., Northeastern Univ., Shenyang, China (Jinda Liu) \|\| State Key Lab. of Robot., Shenyang Inst. of Autom., Shenyang, China (Juntong Qi)
Abstract	In this paper, according to many kinds of hardware-in-the-loop (HIL) simulation systems, especially for the one setting controller as the hardware part, a general HIL development platform was constructed. This platform is consisted of serial input and output communication models, which can be widely used in many kinds of Unmanned Aerial Vehicle (UAV) HIL simulation systems. Changing the UAV model in Simulink and control algorithm in hardware, a new HIL simulation model will be built. This paper references a HIL simulation platform for Rotary-Wing Unmanned Aerial Vehicle (RUAV) developed by Shenyang Institute of Automation, Chinese Academy of Science, then properly modified the communication models and successfully applied them on the Fixed-Wing UAV (FUAV) HIL simulation platform. The HIL method is an effective way to construct a more realistic development platform. The system constructed in this paper not only uses the hardware equipment as the control unit, but also represents the FUAV dynamics model in the Matlab/Simulink environment. Besides, this system also brings in the FlightGear interfacing software to help testers obviously observe the flight state changes. This development pattern brings many advantages for developing the flight dynamics models and controllers of different kinds of UAVs. Results from HIL and realistic flight simulation promote the development, improvement, and realization processes of the UAV flight control algorithms and meanwhile assess the adequacy of the flight model.
Sponsorship	IEEE Syst., Man, Cybern. Soc.
Starting Page	432
Ending Page	437
File Size	304511
Page Count	6
File Format	PDF
e-ISBN	9781479903337
DOI	10.1109/CAC.2013.6775773
Language	English
Publisher	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Publisher Date	2013-11-07
Publisher Place	China
Access Restriction	Subscribed
Rights Holder	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Subject Keyword	FlightGear Software packages Atmospheric modeling Data models Hardware HIL development platform UAV Aircraft Aerospace control
Content Type	Text
Resource Type	Article

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