Automatic Landing Control of Outdoor Blimp Robots(Mechanical Systems)
نویسندگان
چکیده
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 کاملAutomatic 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 کاملautomatic 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 کاملInverse Optimal Velocity Field Control of an Outdoor Blimp Robot
Abstract: A surveillance system is required to gather the suffering information in the stricken area safely and quickly after natural disasters. An autonomous blimp is the best option for this purpose. Inverse optimal velocity field control is proposed for the blimp to keep a desired trajectory. The desired trajectory based on velocity field is designed, and inverse optimal tracking control is ...
متن کاملAutomatic Landing of Small Helicopters on 4 DOF Moving Platforms
In this research, an automatic control system is designed for landing of a small helicopter on a 4 DOF moving platform. The platform has three translational and one directional degree of freedom. The controller design approach is based on development of helicopter nonlinear dynamic model into the SDC (State Dependent Coefficient) form and real time solving of state dependent Riccati equation (S...
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ژورنال
عنوان ژورنال: TRANSACTIONS OF THE JAPAN SOCIETY OF MECHANICAL ENGINEERS Series C
سال: 2010
ISSN: 0387-5024,1884-8354
DOI: 10.1299/kikaic.76.3603