Title :
Simulation and Evaluation Models of Aircraft Power Supply System Based on Simulink /LabVIEW
Author :
Chang Wang ; Jian Huang
Author_Institution :
Sch. of Autom. Sci. & Electr. Eng., Beihang Univ., Beijing, China
Abstract :
Nowadays, aircraft power supply system develops towards multi-electrical direction and digital simulation technology has been widely used. How to rapidly and accurately evaluate the simulation model plays an important role in improving its quality and needs further investigation. In this paper, simulation and evaluation models of aircraft power supply system was studied. Firstly, performance parameters and standards assessing power supply system were confirmed based on GJB181A-2003. A platform evaluating aircraft power supply system was built by means of LabVIEW software. Then, a power supply system simulation model using Simulink platform was built to validate designed evaluation model. Finally, physical prototype test and assessment test of the simulation model verified the feasibility and effectiveness of this evaluation model.
Keywords :
aerospace computing; aerospace simulation; aircraft power systems; digital simulation; power engineering computing; power supplies to apparatus; virtual instrumentation; GJB181A-2003; Simulink-LabVIEW software; aircraft power supply system evaluation models; aircraft power supply system simulation model; digital simulation technology; multielectrical direction; physical prototype test; simulation model assessment test; Aircraft; Analytical models; Atmospheric modeling; Integrated circuit modeling; Load modeling; Mathematical model; Power supplies; LabVIEW; Simulink; aircraft power supply system; evaluation platform; simulation model;
Conference_Titel :
Instrumentation and Measurement, Computer, Communication and Control (IMCCC), 2014 Fourth International Conference on
Conference_Location :
Harbin
Print_ISBN :
978-1-4799-6574-8
DOI :
10.1109/IMCCC.2014.25
