nxControl instead of pitch-and-power
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  • 作者:Simon Müller ; Karolin Schreiter ; Dietrich Manzey…
  • 关键词:Total energy angle ; Potential flight path angle ; Augmented manual flight control ; Thrust control ; Cockpit displays ; Scanning behaviour
  • 刊名:CEAS Aeronautical Journal
  • 出版年:2016
  • 出版时间:March 2016
  • 年:2016
  • 卷:7
  • 期:1
  • 页码:107-119
  • 全文大小:1,104 KB
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    16.Schreiter, K., Müller, S., Luckner, R.: nxControl: Konzept zur Vorgaberegelung für die Längsbeschleunigung des Flugzeugs. Deutscher Luft- und Raumfahrtkongress (2013)
  • 作者单位:Simon Müller (1)
    Karolin Schreiter (2)
    Dietrich Manzey (1)
    Robert Luckner (2)

    1. Work, Engineering and Organisational Psychology - F7, Technische Universität Berlin, Marchstraße 12, 10587, Berlin, Germany
    2. Flight Mechanics, Flight Control and Aeroelasticity - F5, Technische Universität Berlin, Marchstraße 12, 10587, Berlin, Germany
  • 刊物主题:Aerospace Technology and Astronautics;
  • 出版者:Springer Vienna
  • ISSN:1869-5590
文摘
A command system for manual control of the longitudinal load factor in flight path direction of an aircraft is designed that completes existing flight control command systems (e.g. with sidesticks that command normal load factor). The system is called nxControl. It aims to assist pilots during manual flight by reducing the workload for monitoring flight parameters as well as for controlling thrust and airbrakes. Important for the nxControl concept is the direct flight mechanical relation between longitudinal load factor and changes of the total aircraft energy. This paper presents the system concept and a prototype realization. The nxControl system consists of the control law that combines the actuation commands for engines and airbrakes, a new input device for the longitudinal load factor command and augmented display elements informing pilots about aircraft energy states to assure situation awareness. In order to investigate the feasibility of the concept as well as to evaluate consequences on human performance, a flight simulator study with airline pilots was conducted. The nxControl prototype was used by the pilots as expected. Changes in instrument scanning behaviour and thrust lever usage confirmed this. After just a short familiarization and practice, the pilots were able to perform standard flight tasks with nxControl without exceeding given tolerance limits. So, the results provide first evidence for the feasibility of the concept.

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