The problem of synthesizing the pitch angle control system with the angle of attack limiting channel is considered. The problem of matching the trajectories of the system of the pitch angle control mode and the angle of attack limitation mode is discussed. An approach is proposed based on using a generalized characteristic of the system, which ensures the matching the states at an arbitrary moment of change of its operation mode.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Synthesis of Pitch Angle Control System with Angle of Attack Limiting Channel


    Additional title:

    Russ. Aeronaut.


    Contributors:

    Published in:

    Russian Aeronautics ; 63 , 1 ; 25-32


    Publication date :

    2020-01-01


    Size :

    8 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English




    AIRCRAFT PITCH ANGLE AND LIMITING PARAMETERS AUTOMATIC CONTROL SYSTEM

    PETUNIN VALERIJ IVANOVICH / NEUGODNIKOVA LJUBOV MIKHAJLOVNA / ABDULLINA EHL ZA JUNIROVNA | European Patent Office | 2015

    Free access

    PITCH ANGLE CONTROL SYSTEM, PITCH ANGLE CONTROL METHOD, AND VEHICLE

    MIKI MASAYUKI | European Patent Office | 2018

    Free access

    PITCH ANGLE CONTROL SYSTEM, PITCH ANGLE CONTROL METHOD, AND VEHICLE

    MIKI MASAYUKI | European Patent Office | 2015

    Free access

    AUTOMATIC CONTROL SYSTEM OF PITCH ANGLE AND LIMITATION OF ANGLE OF ATTACK OF AIRCRAFT

    PETUNIN VALERIJ IVANOVICH / NEUGODNIKOVA LYUBOV MIKHAJLOVNA / KINZIKEEV TIMUR DANILOVICH | European Patent Office | 2019

    Free access

    Roll-pitch-yaw integrated μ-synthesis for high angle-of-attack missiles

    Choi, Byunghun / Kang, Seonhyeok / Kim, H. Jin et al. | Elsevier | 2011