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Publication date: 27 November 2024

Grzegorz Drupka, Piotr Grzybowski, Piotr Szczerba and Lesław Bichajło

This paper aims to present research carried out on the influence of GUI graphical elements design for an integrated mission management system (IMMS) display flight planning…

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Abstract

Purpose

This paper aims to present research carried out on the influence of GUI graphical elements design for an integrated mission management system (IMMS) display flight planning process.

Design/methodology/approach

Surveys and research were conducted among students/pilots to explore graphic presentation methods for flight planning displays. Guidelines for graphical layout of the IMMS flight planning interface are proposed.

Findings

A research concept was obtained, enabling GUI tests for IMMS using prepared templates and questionnaires.

Practical implications

This study improves cockpit information readability, understanding and presentation, particularly for flight planning elements such as terrain, weather, traffic and zones influencing route organisation.

Social implications

This study targets possible improvements to the flight path planning process in aviation, inducing a reduction in errors related to human factors while processing the visual data on-board.

Originality/value

The study verified the impact of drawing and rendering methods on IMMS flight planning, suggesting that current display methods may be error-prone when showing hazard information from multiple sources on a single screen.

Details

Aircraft Engineering and Aerospace Technology, vol. 97 no. 1
Type: Research Article
ISSN: 1748-8842

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Article
Publication date: 13 April 2020

Paweł Rzucidło, Tomasz Rogalski, Grzegorz Jaromi, Damian Kordos, Piotr Szczerba and Andrzej Paw

The purpose of this paper is to describe simulation research carried out for the needs of multi-sensor anti-collision system for light aircraft and unmanned aerial vehicles.

119

Abstract

Purpose

The purpose of this paper is to describe simulation research carried out for the needs of multi-sensor anti-collision system for light aircraft and unmanned aerial vehicles.

Design/methodology/approach

This paper presents an analysis related to the practical possibilities of detecting intruders in the air space with the use of optoelectronic sensors. The theoretical part determines the influence of the angle of view, distance from the intruder and the resolution of the camera on the ability to detect objects with different linear dimensions. It has been assumed that the detection will be effective for objects represented by at least four pixels (arranged in a line) on the sensor matrix. In the main part devoted to simulation studies, the theoretical data was compared to the obtained intruders’ images. The verified simulation environment was then applied to the image processing algorithms developed for the anti-collision system.

Findings

A simulation environment was obtained enabling reliable tests of the anti-collision system using optoelectronic sensors.

Practical implications

The integration of unmanned aircraft operations in civil airspace is a serious problem on a global scale. Equipping aircraft with autonomous anti-collision systems can help solve key problems. The use of simulation techniques in the process of testing anti-collision systems allows the implementation of test scenarios that may be burdened with too much risk in real flights.

Social implications

This paper aims for possible improvement of safety in light-sport aviation.

Originality/value

This paper conducts verification of classic flight simulator software suitability for carrying out anti-collision systems tests and development of a flight simulator platform dedicated to such tests.

Details

Aircraft Engineering and Aerospace Technology, vol. 92 no. 4
Type: Research Article
ISSN: 1748-8842

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