Wyniki wyszukiwania - BazTech

1

Aircraft precision landing using integrated GPS/INS system

Petrovska O., Rechkoska-Shikoska U.

Transport Problems

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2013

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T. 8, z. 1

17--25

EN

The most critical operation for an aircraft to perform is landing. Even in bad weather, more specifically poor visibility, landing becomes virtually impossible of instrument guidance to aid the pilot. The more extreme case occurs when the visibility is near zero and the pilot cannot land the plane manually. This situation requires an automatic landing or precision approach to be performed by the aircraft flight control system in conjunction with a landing/guidance system. This type of guidance has been provided by the integration of the Global Positioning System (GPS) and Inertial Navigation System (INS).

PL

Najbardziej krytyczną operacją do wykonania samolotem jest lądowanie. Podczas złej pogody, zwłaszcza w słabej widoczności, lądowanie staje się prawie niemożliwe. Najbardziej skrajny przypadek występuje, gdy widoczność jest bliska zeru, a pilot nie może wylądować samolotem ręcznie. Ta sytuacja wymaga automatycznego lądowania lub precyzyjnego podejścia do wykonania przez system kontroli lotów samolotowych w połączeniu z systemem wspomagania lądowania. Ten rodzaj wspomagania został zaopatrzony przez integrację z Globalnym Systemem Pozycjonowania (GPS) i Inercyjnym Systemem Nawigacyjnym (INS).

2

The flying didactic laboratory projekt

Tomczyk A.

Research Bulletin / Warsaw University of Technology, Institute of Aeronautics and Applied Mechanics

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1999

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nr 9

145-150

EN

The article presents main thesis of the didactic flying laboratory project. Range of project tasks and basic functions of the system are shown. Paper contains preliminary project of the on-board measuring system, and list of parameters proposed for measuring, processing, displayed on the screen and storing on the on-board computer memory. Set of possible exercises to be able to realization using the flying laboratory, and perspective directions of system development are presented.

3

Uncertainty management methods and tools with applications to aircraft flight control system design

Brusov V., Tiumentsev Y.

Research Bulletin / Warsaw University of Technology, Institute of Aeronautics and Applied Mechanics

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1998

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nr 8

91-96

EN

Almost all kinds of men's activities associated with design, manufacturing and maintenance of complex systems consist of next two main classes of problems: a generation of decision alternative set allowed for situation studied, and decision making, i.e. choice of some decision alternative from the set of allowed ones. A role of various kinds of uncertainties related to complex system design process is discussed based on intelligent flight control system design example. A mixed information technology is used for this problem solving based on mathematical modeling, multi-purpose system methodology and artificial neural networks. This approach promises to stay an effective technical decision generation and making tool for problem solving with various kind of uncertainties involved.

4

Modern problems in manual control of higly augmented aircraft

Efremov A.

Research Bulletin / Warsaw University of Technology, Institute of Aeronautics and Applied Mechanics

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1998

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nr 8

177-180

EN

There is briefly analyzed the new role of flight control system highly augmented aircraft, goals and problems in their design. The system approach based on deep study of regularities in pilot behavior is considered shortly as a tool for the solution of different manual control tasks. The efficiency of the system approach is demonstrated on a number of applied tasks. The specific place is dedicated to the analysis of facilities appropriated to the different stages of experimental investigations on manual control. The high efficiency of the workstation developed for solution of different manual control tasks is shown too.