飞行器管理系统需求  

Vehicle Management System Requirements

作　　者：张勇[1] 

机构地区：[1]沈阳飞机设计研究所,辽宁沈阳110035

出　　处：《飞机设计》2011年第1期71-76,共6页Aircraft Design

摘　　要：飞行器管理系统(VMS)将飞行、推进控制与相关的公管系统综合。飞行器管理系统的概念为性能改善带来了巨大的好处,同时对可靠性、维修性和保障性有重大改善。未来高性能的飞机将具有多操纵面/效应器以保证机动性,利用飞行/推进综合控制实现性能收益。随着更多系统的参与,综合设计的难度会增加。为确保VMS的实际应用,需要明确其计算和结构需求。A Vehicle Management System（VMS） integrates the flight and propulsion control with the related utility systems.The VMS concept offers significant performance benefits as well as major improvements in reliability,maintainability and supportability.Future high performance aircraft will likely be configured with multiple control surfaces/effectors to provide high maneuverability and with an integrated flight/propulsion control system to provide significant performance payoffs.The integration problem increases in difficulty as more systems are added.In order to assure a practical implementation of a VMS,A process is needed to develop the computational and architectural requirements.

关 键 词：飞行器管理系统 飞行/推进综合控制 公管系统 

分 类 号：V241.4[航空宇航科学与技术—飞行器设计]