Hardware-in-the-Loop Simulation of Aerodynamic Objects

Author:

Bacic Marko1,MacDiarmid Monte1

Affiliation:

1. University of Oxford

Publisher

American Institute of Aeronautics and Astronautics

Reference9 articles.

1. 1Klein,V.andMorelli,E.A.AircraftSystemIdentification:TheoryandPractice,AIAAEducationSeries,2006.

2. Contributions of hardware-in-the-loop simulations to Navy test and evaluation

3. 4Sefic,W.J.andMaxwell,C.M.,X29Atechnologydemonstratorflighttestprogramoverview,NASATM-86809,1986. (a) Oxford's low-cost dynamic wind tunnel test facility under development. The system consists of computer controlled free jet windtunnelandacomputercontrolled3-axismotionsimulator (b) Sketch of the purpose developed motion simulator for wind tunnel based hardware-in-the-loop simulation. The motion simulatorhasalowestresonancefrequencyinexcessof30hzandwhen completedwillprovidefullrangeofmotioninroll,yawandpitch

4. 5Mackall,D.A.Qualificationneedsforadvancedintegratedaircraft,NASA-DrydenResearchCentreTM-86731,1985.

5. 6Binkey,R.L.andMackall,D.A.SystemoverviewoftheNASADrydenintegratedtestfacility,NASATM-104250,1992.

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