本文件的目的是为主动驾驶舱控制器（也称为主动接收器）开发感觉力控制系统的一般特性和要求。该文件介绍了描述这些类型系统的推荐关键特性和设计考虑因素的技术材料。在适当的情况下，明确识别平台特定要求（例如，单轴/双轴、单座/双座、民用/军用、旋翼机/固定翼飞机等）的影响。 开发的材料将作为以下方面的参考指南: 一个 希望了解主动座舱控制器技术并开发自己的一套要求的飞机主承包商； b 开发主动驾驶舱控制器设备的供应商； c 将参与这些类型系统认证的监管机构。

The purpose of this document is to develop the general characteristics and requirements for feel-force control systems for active cockpit controllers, also known as Active Inceptors. The document presents technical material that describes the recommended key characteristics and design considerations for these types of systems. Where appropriate, the effects of platform specific requirements (e.g., single axis/dual axis, single seat/dual seat, civil/military, rotorcraft/fixed wing aircraft, etc.) are clearly identified. The material developed will serve as a reference guide for: a Aircraft prime contractors who want to understand active cockpit controller technology and develop their own set of requirements; b Suppliers that develop active cockpit controller equipment and; c Regulatory Authorities who will be involved in the certification of these types of systems.