The Challenge: Designing a light-weight, low-cost control and data system for the engine controller and a remote data system for propellant conditioning for an Air Force SBIR Phase III vortex propulsion flight demonstration program. The Solution: Developing a low cost, off-the-shelf embedded system with minimal manpower and increased flexibility using a custom NI LabVIEW application and the NI CompactRIO platform to deterministically control a liquid rocket engine and its associated feed systems. Additionally developing an easy to setup remote temperature monitoring system.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Real-Time Flight Engine Controller Using NI LabVIEW and CompactRIO Hardware


    Contributors:
    J. Hoopes (author)

    Publication date :

    2011


    Size :

    6 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English





    Balancing scooter meets NI compactRIO

    Werth, Wolfgang | Tema Archive | 2006


    Implementation of Space Vector Pulse Width Modulation using CompactRIO

    Yusivar, Feri / Sembiring, Reynhard Josian | IEEE | 2013


    Datenerfasssung und Fernzugriff mit CompactRIO in Omnibussen

    Bach, Peter / Bahlmann, Norbert / Koerver, Wolfram | Tema Archive | 2008


    Integrated Control of Engine Dynamometer Using LabVIEW Platform - Hardware

    de Luca, A.M. / Victorette, M. / Vandresen, M. et al. | British Library Conference Proceedings | 2011