Hardware-In-The-Loop Power Extraction Using Different Real-Time Platforms (Postprint)

Abstract

Aircraft power demands continue to increase with the increase in electrical subsystems. These subsystems directly affect the behavior of the power and propulsion systems and can no longer be neglected or assumed linear in system analyses. The complex models designed to integrate new capabilities have a high computational cost. Hardware-in-the-loop (HIL) is being used to investigate aircraft power systems by using a combination of hardware and simulations. This paper considers three different real-time simulators in the same HIL configuration. A representative electrical power system is removed from a turbine engine simulation and is replaced with the appropriate hardware attached to a 350 horsepower drive stand. Variables are passed between the hardware and the simulation in real-time to update model parameters and to synchronize the hardware with the model. Real-time simulation platforms from dSPACE, National Instruments (NI), and the MathWorks' xPC are utilized for this investigation. Similar results are obtained when using HIL and a simulated load. Initially, noticeable differences are seen when comparing the results.

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Document Details

Document Type
Technical Report
Publication Date
Nov 01, 2008
Accession Number
ADA506389

Entities

People

  • John Mcnichols
  • Michael Boyd
  • Michael Corbett
  • Mitch Wolff
  • Peter Lamm

Tags

Communities of Interest

  • Air Platforms
  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Air Force
  • Air Force Research Laboratories
  • Aircrafts
  • Control Systems
  • Data Sets
  • Engine Components
  • Extraction
  • Generators
  • Mach Number
  • Military Research
  • Operating Systems
  • Platforms
  • Propulsion Systems
  • Simulations
  • Simulators
  • Steady State
  • Turbines

Readers

  • Electrical Engineering
  • Software Engineering.
  • Unmanned Aerial System (UAS) Autonomous Capabilities and Mission Reconnaissance.