This software models a propulsive reaction control system (RCS) for guidance, navigation, and control simulation purposes. The model includes the drive electronics, the electromechanical valve dynamics, the combustion dynamics, and thrust. This innovation follows the Mars Science Laboratory entry reaction control system design, and has been created to meet the Mars Science Laboratory (MSL) entry, descent, and landing simulation needs. It has been built to be plug-and-play on multiple MSL testbeds [analysis, Monte Carlo, flight software development, hardware-in-the-loop, and ATLO (assembly, test and launch operations) testbeds]. This RCS model is a C language program. It contains two main functions: the RCS electronics model function that models the RCS FPGA (field-programmable-gate-array) processing and commanding of the RCS valve, and the RCS dynamic model function that models the valve and combustion dynamics. In addition, this software provides support functions to initialize the model states, set parameters, access model telemetry, and access calculated thruster forces.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Propulsive Reaction Control System Model


    Beteiligte:


    Erscheinungsdatum :

    01.11.2011


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Propulsive lander control system

    Mankovitz, R. J. | NTRS | 1965


    VEHICLE PROPULSIVE FORCE CONTROL SYSTEM

    IMAMURA TATSUYA / KOMADA HIDEAKI / NISHIMINE AKIKO et al. | Europäisches Patentamt | 2019

    Freier Zugriff

    Propulsive system

    REBHI BETKA / RAFFAELLI LORENZO / ROLT ANDREW MARTIN | Europäisches Patentamt | 2016

    Freier Zugriff

    FLUIDIC PROPULSIVE SYSTEM

    ANDREI EVULET | Europäisches Patentamt | 2024

    Freier Zugriff

    Fluidic propulsive system

    EVULET ANDREI | Europäisches Patentamt | 2023

    Freier Zugriff