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Pilot-Centered Design of a Longitudinal Acceleration Command System for Augmented Manual Flight Control (nx-Control)

以飞行员为中心的增强手动飞行控制纵向加速指令系统（nx-Control）设计

基本信息

批准号：
225630728
负责人：
Professor Dr.-Ing. Robert Luckner
金额：
--
依托单位：
Fachgebiet Flugmechanik, Flugregelung und Aeroelastizität
依托单位国家：
德国
项目类别：
Research Grants
财政年份：
2012
资助国家：
德国
起止时间：
2011-12-31 至 2018-12-31
项目状态：
已结题

来源：
https://gepris.dfg.de/gepris/projekt/225630728?language=en
关键词：
Pilot Centered Design Longitudinal Acceleration

项目摘要

The growing air traffic increases the requirements on pilots with respect to flight control. It is expected that more complex trajectories are to be aviated with greater precision than today. This will not be a problem in case of automated flying. However, the increased requirements, in principle, must also remain achievable even in manual flight. This means higher cognitive and motoric workload of the pilots compared to today, due to more complex energy management. Thus far, the manual control of thrust and speed brakes, the elements that influence the airplane's total energy, is based on so called pitch-and-power estimations. In today's cockpits, there is no support for this task. This is in contrast to already available augmented flight control systems for controlling the aircraft's attitude. In the first project phase, the requirements resulting from the management of energies and the involved cognitive processes of pilots were investigated. On this basis a new flight controller for the longitudinal load factor was developed (nxControl) to assist the pilot by combining the energy increasing and decreasing elements in one command. Thereby, the controller significantly reduces the cognitive and motoric workload of pilots in manual flight. Parallel to this development, also a new control lever and several display enhancements were developed in a pilot-centered approach to visualize the functioning of the system and to make its operation as intuitive as possible. In a flight simulator study it could already be shown that the nxControl system is comprehensible and well accepted by the pilots. In addition, it could be proved that today's standard flight tasks can be managed with nxControl at a lower workload with similar precision, compared to conventional manual flight. Thus, the main goals of the first project phase have been achieved. The objective of the second project phase is to show that the nxControl concept can be integrated coherently into the existing cockpit philosophy of today's commercial aircraft for the entire flight from gate to gate. This will be done in three steps. First, the system will be expanded and completed according to the requirements of the transition from flight to ground mode. In ground mode the new controller can access wheel brakes and thrust reverser to reduce energy. Second, it will be investigated in a simulator study whether the system can still operate in case of energy-related failures (e.g. engine failure) and still provide effective support to the pilot. Based on the results, if necessary, the system will be further optimized. Third, it will finally be demonstrated that, given the new system, also complex future flight trajectories can still be aviated in manual mode with reasonable accuracy and moderate workload. For this purpose, the integrated system including the controller and new cockpit interfaces will be evaluated in a comprehensive flight simulator study with licensed airline pilots.

不断增长的空中交通量增加了对飞行员在飞行控制方面的要求。预计将以比今天更高的精度飞行更复杂的轨道。在自动化飞行的情况下，这不会是一个问题。然而，原则上，即使在手动飞行中，也必须能够实现增加的要求。这意味着与今天相比，由于更复杂的能量管理，飞行员的认知和运动负荷更高。到目前为止，推力和速度制动器的手动控制，影响飞机的总能量的元素，是基于所谓的俯仰和功率估计。在今天的驾驶舱里，没有人支持这项任务。这与已经可用的用于控制飞机姿态的增强飞行控制系统形成对比。在第一个项目阶段，所产生的能源管理和飞行员的认知过程的要求进行了调查。在此基础上，开发了一种新的纵向载荷因子飞行控制器（nxControl），通过在一个命令中组合能量增加和减少元件来辅助飞行员。因此，控制器显著降低了手动飞行中飞行员的认知和运动负荷。与此同时，还开发了一个新的控制杆和几个显示增强功能，以飞行员为中心的方法来可视化系统的功能，并使其操作尽可能直观。在飞行模拟器研究中，已经可以证明nxControl系统是可以理解的，并且被飞行员很好地接受。此外，可以证明，与传统的手动飞行相比，nxControl可以以更低的工作负载和类似的精度管理当今的标准飞行任务。因此，项目第一阶段的主要目标已经实现。项目第二阶段的目标是证明nxControl概念可以连贯地集成到当今商用飞机的现有驾驶舱理念中，用于从登机口到登机口的整个飞行。这将分三步完成。首先，系统将根据从飞行模式到地面模式过渡的要求进行扩展和完成。在地面模式下，新控制器可以访问车轮制动器和推力反向器以减少能量。第二，将在模拟器研究中调查该系统在与能量有关的故障（例如发动机故障）的情况下是否仍然能够运行，并且仍然为飞行员提供有效的支持。根据结果，如有必要，将进一步优化系统。第三，最终将证明，在新系统的情况下，未来复杂的飞行轨迹仍然可以在手动模式下以合理的精度和适度的工作量进行飞行。为此，包括控制器和新的驾驶舱接口在内的综合系统将在有执照的航空公司飞行员的综合飞行模拟器研究中进行评估。