Purpose

A standard automatic flight control system – autopilot – will become required equipment of the future aircraft, operating in the common sky. For a specific group of aircraft, they are too expensive and too energy-consuming solutions. This paper aims to present the concept of an automatic flight control system that overcomes those limitations.

Design/methodology/approach

The proposed automatic flight control system uses the trim tabs in all prime flight controlling surfaces: elevator, ailerons and rudder, for stabilizing and controlling the steady flights of an aircraft.

Findings

The results of an aeroplane flight controlled with the use of trim tabs simulation tests and remarks have been presented and discussed. The simulation was conducted in real-time hardware in the loop environment. The stabilization of the flight was achieved in performed test scenarios.

Originality/value

The possibility to control an aircraft with coordinated deflections of the trimming surfaces is a beneficial alternate to those currently used and can be recommended for use in the next-generation aircraft.

中文翻译：

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飞机装饰系统–新功能

目的

标准的自动飞行控制系统-自动驾驶仪-将成为未来飞机在普通空中运行的必需设备。对于特定的飞机组，它们太昂贵且太耗能。本文旨在提出克服这些限制的自动飞行控制系统的概念。

设计/方法/方法

拟议中的自动飞行控制系统在所有主要飞行控制表面（升降舵，副翼和方向舵）中均使用装饰翼片，以稳定和控制飞机的稳定飞行。

发现

已经介绍和讨论了通过使用装饰片模拟测试和备注来控制飞机飞行的结果。仿真是在循环环境中的实时硬件中进行的。在执行的测试场景中实现了飞行的稳定。

创意/价值

可以控制飞机的纵倾面的挠度，这是对当前使用的飞机的一种有益替代，可以推荐用于下一代飞机。