Wyniki wyszukiwania - BazTech

1

Budowa regułowego modelu systemu sterowania samolotem TS-11 ISKRA

Golański P., Szkudlarz H.

Pomiary Automatyka Robotyka

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2009

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R. 13, nr 2

633-639

PL

W artykule przedstawiono metodę tworzenia modelu sterowania samolotem przez pilota. W pracy skupiono się na realizacji procedury startu. W tym celu wykorzystano instrukcje wykonywania lotu oraz wiedzę pilota. Na zakończenie przedstawiono postać regułowego modelu systemu sterowania samolotem oraz wyniki przeprowadzonych symulacji.

EN

This paper presents the method of building of aircraft control model. Here, the focus is on the model of taking off procedure. For this purpose the fly instruction and pilot knowledge has been used. Finally, the model formalization and simulation results, has been presented.

2

Aircraft control system modyfing plane's flying characteristics to simulate another plane's behavior

Rogalski T., Dołęga B.

Zeszyty Naukowe Politechniki Rzeszowskiej. Mechanika

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2004

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z. 62 [209]

329--340

EN

According to new idea of aircraft controlling, the main tasks of the control system mounted on the board are to augment aircraft stability, to reduce pilot's load, to protect plane against dangerous states of fly. Generally the flying with small local transport airplane should be both safer and more pleasant. The system is going to meet its main goals changing aircraft behavior toward behavior of planes recognized as easy to fly with. Model following idea was used to prepare control laws, allowing simulating another plane dynamics. This report intends to present both general conception and practical realization of control system destined for small aircraft. Described system is planned to be installed on the board of PZL M 20 typical for that group of airplanes. Several tests of designed system including tests allowing to get know pilots' opinion about new modes of stick's operation were performed.

3

Aircraft control system enabling fly for everybody

Rogalski T., Dołęga B.

Zeszyty Naukowe Politechniki Rzeszowskiej. Mechanika

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2004

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z. 62 [209]

319--328

EN

This report intends to present both general conception and a few aspects of practical realization of control system destined for small general aviation aircraft. Described system is planned to be installed on the board of PZL M 20 typical for this group of airplanes. According to the new idea of aircraft controlling, the main tasks of the control system mounted on the board are to augment aircraft stability, to reduce pilot's load, to protect plane against dangerous states of fly. Generally the flying with small local transport airplane should be both safer and more pleasant. The system going to meet its main goals uses semi-intelligent stick or side-stick to control plane. There are few main modes of the stick's working. In classical mode it works like in normal plane. There is a geometrical relation beetween position of stick to position of actuators.

4

System sterowania samolotem z zastosowaniem magistrali CAN

Pieniążek J.

Szybkobieżne Pojazdy Gąsienicowe

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2003

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nr 1 (17)

33-40

PL

Sterowanie samolotem wymaga wielu informacji, które we współczesnych systemach mają postać cyfrową. W ramach prowadzonych prac badawczych nad system pośredniego sterowania, realizowanym w Katedrze Awioniki i Sterowania PRz, poszukiwane są nowe rozwiązania dla lotnictwa. Jednym z tych rozwiązań jest koncepcja zastosowania magistrali CAN do przesyłania informacji pomiędzy urządzeniami pomiarowymi, sterującymi i prezentującymi informacje dla pilota. W artykule zostały zaprezentowane wybrane aspekty rozwiązania lotniczego systemu sterowania z zastosowaniem magistrali CAN.

EN

In the aircraft control process many digital data is used. Research on the control system and associated measurement devices is implemented in the Department of Avionics and Control of Rzeszow Technical University. One of applied solution is CAN bus using in the Augmented Control System for easy piloted aircraft. Measurement and control devices used in recent project are equipped with CAN interface. Some aspects of this solution are presented in the paper including: hardware configuration, interface states definition and system monitoring.