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2016, vol. 64, iss. 3, pp. 838-849
Open loop control of the five-axis missile and target flight motion simulator implementation
Military Technical Institute - MTI, Belgrade,,
Keywords: tests; simulations; missiles; data acquisition; signal generation; state machine; synchronized measurements; LabVIEW; hardware in the loop
An important phase in missile systems development is flight testing and simulation in the environmental conditions dictated by the operation the system is made for. Since field testing of complex systems means a big financial burden and a time consuming process, hardware in the loop (HIL) simulations represent a very effective solution for saving both costs and time. This paper presents an implementation of a control application that integrates synchronized data generation and acquisition on the five-axis missile and target flight motion simulator owned by the HIL laboratory. The described simulation application is a result of a missile development engineer's need for a simple way to acquire information on a real missile response, when desired control signals are provided. The solution is realized in Lab VIEW software using a robust software design architecture named 'classic state machine'.
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Bress, J.T. (2013) Effective LabVIEW Programming
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National Instruments (2012) LabView Data Acquisition and Signal Conditioning, Course Manual
National Instruments (2008) NI-Tutorial-3567, LabVIEW FPGA in Hardware in-the- Loop Simulation Applications
Oberkampf, W.L., DeLand, S.M., Rutherford, B.M., Diegert, K.V., Alvin, K.F. (2002) Error and uncertainty in modeling and simulation. Reliability Engineering & System Safety, 75(3): 333-357
USA, Department of Defense (1995) Military Handbook, Missile Flight Simulation, Part One, Surface - To - Air Missiles. MIL-HDBK-1211, MI


article language: English
document type: Professional Paper
DOI: 10.5937/vojtehg64-9493
published in SCIndeks: 11/06/2016
peer review method: double-blind
Creative Commons License 4.0

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