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 کاملModeling of the Human Pilot in Aircraft Landing Control
This paper provides an overview of literature on visual perception for position and motion awareness in general, and focuses on the visual inputs used by human pilots for landing aircraft in particular. General introductions are given on the background of manual aircraft landing and on depth and motion perception. These fields are then brought together in a discussion of visual cues available d...
متن کاملThe Role of Binocular Cues in Human Pilot Landing Control
The paper discusses the possible use of binocular cues by aircraft pilots in the final landing phase through a review of literature. The review includes medical and psychophysical literature, as well as works on pilot training, certification and flight experiments. It was found that stereopsis can be used as a depth cue up to several hundred meters. However, in situations where monocular cues a...
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: The Japanese journal of ergonomics
سال: 1970
ISSN: 0549-4974,1884-2844
DOI: 10.5100/jje.6.157