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Aerospace - Vehicle Management Systems - Flight Control Design, Installation and Test of, Military Unmanned Aircraft, Specification Guide For 航空航天 - 车辆管理系统 - 军用无人机飞行控制设计 安装和测试 规格指南
发布日期: 2012-12-19
本文件为军用无人驾驶飞机(UA)的车辆管理系统(VMS)的飞行控制相关功能的一般性能、设计、测试、开发和质量保证要求的规范建立了推荐实践,UA是无人驾驶飞机系统(UAS)的机载元件,如ASTM F 2395-07所定义。该文件是为主要用于军事行动领域的军用无人驾驶飞机编写的。该文件还为适用于所有类别空域安全飞行的考虑提供了基础。
This document establishes recommended practices for the specification of general performance, design, test, development, and quality assurance requirements for the flight control related functions of the Vehicle Management Systems (VMS) of military Unmanned Aircraft (UA), the airborne element of Unmanned Aircraft Systems (UAS), as defined by ASTM F 2395-07. The document is written for military unmanned aircraft intended for use primarily in military operational areas. The document also provides a foundation for considerations applicable to safe flight in all classes of airspace.
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归口单位: AEROC
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