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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。
The aircraft management system (VMS) integrates flight, propulsion control and related public-plumbing systems. The concept of an aircraft management system has brought huge benefits to performance improvement with significant improvements in reliability, maintainability and security. Future high-performance aircraft will have multiple control surfaces / effectors to ensure maneuverability and performance gains with integrated flight / propulsion control. With more systems involved, the complexity of the integrated design will increase. In order to ensure the practical application of VMS, its calculation and structural requirements need to be clearly defined.