nxControl instead of pitch-and-power

nxControl instead of pitch-and-power
复制标题

nxControl 代替音调和功率

DOI:
10.1007/s13272-015-0169-9
复制
发表时间:
--
影响因子:
--
通讯作者:
Luckner
Luckner
中科院分区:
--
文献类型:
--
作者:
Müller;Schreiter;Manzey;Luckner

文献摘要

参考文献

被引文献

相似文献

设计了一种用于手动控制飞机航迹方向纵向载荷率的指挥系统,以完善现有的飞行控制指挥系统(例如,具有控制正常载荷率的侧标)。该系统称为nxControl。它的目的是通过减少监测飞行参数以及控制推力和空气刹车的工作量,帮助飞行员进行手动飞行。对于nxControl概念来说,重要的是纵向载荷系数和飞机总能量变化之间的直接飞行力学关系。本文给出了该系统的概念和一个原型实现。NxControl系统包括结合发动机和空气制动器的启动命令的控制律、用于纵向负载系数命令的新输入设备和增强的显示元件,通知飞行员飞机能量状态以确保态势感知。为了研究这一概念的可行性以及评估对人类表现的影响,对航空公司的飞行员进行了飞行模拟器研究。飞行员们如期使用了nxControl原型。仪器扫描行为和推力杆使用的变化证实了这一点。经过短暂的熟悉和练习,飞行员能够在不超过给定容差限制的情况下使用nxControl执行标准飞行任务。因此,这一结果为这一概念的可行性提供了第一个证据。
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.
全新生态初级飞行显示概念
DOI: 10.1109/dasc.2008.4702820
发表时间: 2008
期刊: 2008 IEEE/AIAA 27th Digital Avionics Systems Conference
影响因子: --
作者:
T. Lambregts;R. Rademaker;E. Theunissen
通讯作者: E. Theunissen
DOI: 10.2514/6.2010-8169
发表时间: 2010
期刊: Autom.
影响因子: --
作者:
P. Rijneveld;C. Borst;M. Mulder;René van Paassen
通讯作者: René van Paassen
先进飞机飞行性能:命名法
DOI: --
发表时间: 2012
期刊:
影响因子: --
作者:
Antonio Filippone
通讯作者: Antonio Filippone
DOI: 10.14279/depositonce-6995
发表时间: 2013
影响因子: --
作者:
S. Müller;K. Schreiter;D. Manzey
通讯作者: D. Manzey
DOI: 10.14279/depositonce-6997
发表时间: 2013
期刊: The International Journal of Aviation Psychology
影响因子: --
作者:
S. Müller;D. Manzey;Anne Bleyer;K. Schreiter;A. Voigt;R. Luckner
通讯作者: R. Luckner