This article presents flight tests of a newly developed Helmet-Mounted Flight Parameters Display System (SWPL). Presented system is designed to illustrate full piloting and navigational information, warning about emergency on the helicopter’s board and signaling on-board helicopter systems failures on the translucent display. The system is designed to work in day and night time conditions. In night time conditions, the system cooperates with night vision goggles applicable in Polish Air Force. The article presents the main components of the tested system, along with their purpose and function. It also describes in detail the methods of display implemented in the system and the amount of displayed information. The article discusses the required range and the actual course of the flight tests of that system. Tests were conducted on a Mi-17-1V helicopter. The results of the flight tests of the Helmet-Mounted Display System are given in conclusion, in particular regarding meeting the tactical and technical requirements of the system.


    Access

    Download


    Export, share and cite



    Title :

    Flight Parameter Display System For The Mi-17 Helicopter – Test Results




    Publication date :

    2015




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    Unknown




    MI-38 Helicopter Flight Test Results

    Samusenko, A. / Pavlenko, N.S. / Chalov, N.I. et al. | British Library Conference Proceedings | 2007


    Multimission helicopter display subsystem: transition to flight test

    Green, Dale C. / Terry, William S. | SPIE | 1997


    Flight Test Results NH90 NFH Helicopter-Ship Qualification Process

    Hoencamp, A. / Pavel, M.D. / Vertical Flight Technical Society | British Library Conference Proceedings | 2012


    Helicopter flight test instrumentation

    Ferrell, K. R. | TIBKAT | 1980


    Automatic Flight Control System for an Unmanned Helicopter System Design and Flight Test Results

    Weidel, M. / Alles, W. / Advisory Group for Aerospace Research and Development; Flight Mechanics Panel | British Library Conference Proceedings | 1995