Aerospace vehicle is connected to the ground system through umbilical connectors. Before connecting the umbilical connectors to the flight worthy system, it is essential to test and cleared the ground system. Umbilical Test Jig (UTJ) with passive resistors is not able to simulate the actual power of aerospace vehicle subsystems. The Automated Umbilical Test Jig (AUTJ) incorporates a programmable electronic load which can simulate the actual power requirement of aerospace vehicle sub-systems and measure the values. The present paper deals with design and realization of Programmable Electronic Load (PEL) based on active load and microcontroller (MSP430F6659).


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Design and Realization of Programmable Electronic Load for Aerospace Vehicle Testing


    Beteiligte:
    Kumar, Kamlesh (Autor:in)


    Erscheinungsdatum :

    22.07.2024


    Format / Umfang :

    1242334 byte




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



    Testing Electric Vehicle Sub-Systems Using Low Cost Programmable Electronic Load

    Gambhir, Ameya V / Doctor, Nekzad | SAE Technical Papers | 2019


    Testing Electric Vehicle Sub-Systems Using Low Cost Programmable Electronic Load

    Gambhir, Ameya V. / Doctor, Nekzad | British Library Conference Proceedings | 2019


    Aerospace vehicle design

    Wood, K. D. | SLUB | 1963


    Lightening the load for aerospace design

    Emerald Group Publishing | 2002


    Electronic Load Evaluation for Aerospace Power System Verification

    D. Sadey / N. Carbone / K. Boomer et al. | NTIS | 2023