In this paper a novel terminal guidance law for hypersonic vehicle is investigated. In order to accelerate the convergence rate of line of sight angle, adding a power integrator technique based nonlinear guidance law which can make the line of sight converge to zero in finite time is proposed. Then rigorous stability analysis of finite-time convergence is shown. It demonstrates the effectiveness of the approach by numerical simulation meanwhile the approach have strong robustness in the presence of disturbance.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Adding a power integrator technique based terminal guidance law


    Contributors:
    Wang, Songyan (author) / Sun, Xiangyu (author) / Chao, Tao (author) / Ma, Ping (author)


    Publication date :

    2016-08-01


    Size :

    206231 byte




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English




    Roll offset sideslip-turn terminal guidance with rudder integrator feedback

    MICHENER DREW DAVID / DAVIS SCOTT DAVID | European Patent Office | 2024

    Free access

    ROLL-BIASED SKID-TO-TURN TERMINAL GUIDANCE WITH RUDDER INTEGRATOR FEEDBACK

    MITCHNER DREW DAVID / DAVIS SCOTT DAVID | European Patent Office | 2025

    Free access

    ROLL-BIASED SKID-TO-TURN TERMINAL GUIDANCE WITH RUDDER INTEGRATOR FEEDBACK

    MITCHNER DREW DAVID / DAVIS SCOTT DAVID | European Patent Office | 2022

    Free access

    ROLL-BIASED SKID-TO-TURN TERMINAL GUIDANCE WITH RUDDER INTEGRATOR FEEDBACK

    MITCHNER DREW / DAVIS SCOTT | European Patent Office | 2023

    Free access