Ordinary the control system of the aerospace vehicle (ASV) is designed basing on itself linear system. However, there are some non-linear parts in the actuator which can effects flight attitude control. Using the methods of analyzing linear system cannot identify the factors influencing the control system. This paper use description function to analyze the effects for control system. On that basis, this paper put forward a new approach which changes control system by adding series leading correction and reducing gain. Meanwhile, this article proposed an optimal design scheme considering nonlinearity of ASV.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    The Effects and Design Optimization of Backlash Nonlinearity in the Actuator of Aerospace Vehicle


    Contributors:
    mingjia, Zhu (author) / zhiyong, She (author)


    Publication date :

    2020-11-27


    Size :

    1490561 byte




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English



    Rear Derailleur Anti-Backlash Electrical Actuator

    HAMED HAZEM NIHAD | European Patent Office | 2023

    Free access

    ANTI-BACKLASH FLIGHT CONTROL ACTUATOR SYSTEM

    AHYOW BERNARD | European Patent Office | 2021

    Free access

    Anti-Backlash Flight Control Actuator System

    AHYOW BERNARD | European Patent Office | 2024

    Free access

    Backlash measurement system for an electromechanical actuator

    GOHIL AAKASH / ELLIS ANDREW MICHAEL / KLIM GRAEME PETER ARTHUR et al. | European Patent Office | 2023

    Free access