Fixed-time control for automatic carrier landing with disturbance

نویسندگان
چکیده

برای دانلود رایگان متن کامل این مقاله و بیش از 32 میلیون مقاله دیگر ابتدا ثبت نام کنید

اگر عضو سایت هستید لطفا وارد حساب کاربری خود شوید

منابع مشابه

Automatic Landing Guidance Systems and Design of an Optimal Landing Control System

Guidance and control of aircraft in the landing phase imposes extra pilot work loads, hence application of automatic landing control systems is of great importance. In this study automatic landing control systems are introduced and an optimal landing control system is designed. The control system performance criteria are based on minimum control effort. The designed system is simulated for a tr...

متن کامل

Automatic Landing Guidance Systems and Design of an Optimal Landing Control System

Guidance and control of aircraft in the landing phase imposes extra pilot work loads, hence application of automatic landing control systems is of great importance. In this study automatic landing control systems are introduced and an optimal landing control system is designed. The control system performance criteria are based on minimum control effort. The designed system is simulated for a tr...

متن کامل

automatic landing guidance systems and design of an optimal landing control system

guidance and control of aircraft in the landing phase imposes extra pilot work loads, hence application of automatic landing control systems is of great importance. in this study automatic landing control systems are introduced and an optimal landing control system is designed. the control system performance criteria are based on minimum control effort. the designed system is simulated for a tr...

متن کامل

Continuous uniformly finite time exact disturbance observer based control for fixed-time stabilization of nonlinear systems with mismatched disturbances

This paper presents a continuous composite control scheme to achieve fixed-time stabilization for nonlinear systems with mismatched disturbances. The composite controller is constructed in two steps: First, uniformly finite time exact disturbance observers are proposed to estimate and compensate the disturbances. Then, based on adding a power integrator technique and fixed-time stability theory...

متن کامل

Research on automatic landing control for the Jumbo Jet

-----------------------------------------------------------------Abstract--------------------------------------------------------This work mainly focuses on automatic landing control methods for the jumbo jet. The six degree-of-freedom nonlinear model of Boeing707 has been established, using classical control method, gliding beam guidance law, lateral beam guidance law, autoflare guidance law a...

متن کامل

ذخیره در منابع من


  با ذخیره ی این منبع در منابع من، دسترسی به آن را برای استفاده های بعدی آسان تر کنید

ژورنال

عنوان ژورنال: Aerospace Science and Technology

سال: 2021

ISSN: 1270-9638

DOI: 10.1016/j.ast.2020.106403