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Simulated Dynamic Interface Testing as a Tool in the Forecasting of Air Vehicle Deck Limits and Deck Landing Aids

机译:模拟动态界面测试作为空气车辆甲板限制和甲板着陆艾滋病预测的工具

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The use of a 6 degree-of-freedom motion flight simulator to forecast physical deck motion and deck motion limits, is discussed. Full flight test programs using the Merlin CAE Trainer System at RNAS Culdrose and the Manned Flight Simulator at NAVAIRTESTCEN, (Patuxent River, Maryland), are described. Using a real-time ship motion-based helicopter recovery monitoring system (Landing Period Designator or LPD), pilots perform flight-testing evolutions (DLQ). The simulated flight test has five essential objectives: assess the capabilities of the Cockpit Dynamic Simulator (CDS) to support or conduct helicopter-ship operational limits; demonstrate High Level Architecture (HLA) federation; evaluate recovery safety improvements offered by experimental systems, such as the LPD; and determine feasibility of applying these simulators in support of dynamic interface at sea testing. The method, which has been implemented at both centres, gives good performance and correlation with apparent quiescent windows of deck motion. The theoretical approach is described. Results are presented in relation to the stability issues normally confronted by a helicopter at the instant of recovery in progressively difficult conditions. The summaries include development, simulation and testing of various helicopter recovery aids, which were applied during the simulator test. Measurements of instantaneous degree-of-freedom velocity and acceleration are reported, and preliminary comparisons are made with, and between, aided launch and recovery and non-aided evolutions. A brief synopsis of the theory and calculation of the ship motion simulation and Energy Index programs, are discussed. Air vehicle and deck availability are enhanced well beyond the indicated envelope when the operator uses the energy index to signal the top of recovery. As developed in the report, green deck points are identified even in the worst of sea conditions. The periods may be rapid, but owing to the rise time, the deck is constrained to pass from green to red by a latency period.
机译:讨论了使用6自由度运动飞行模拟器来预测物理甲板运动和甲板运动限制。描述了使用Merlin Cae Trainer系统的完整飞行测试计划,在Navairtestcen(Patuxent River,Maryland)中,使用Merlin Cae Trainer系统,并在Navairtestcen(马里兰州)。采用基于实时船舶运动的直升机恢复监控系统(着陆周期指定器或LPD),飞行员执行飞行测试演进(DLQ)。模拟飞行试验有五个基本目标:评估驾驶舱动态模拟器(CDS)的能力,以支持或进行直升机运行限制;展示高级架构(HLA)联合会;评估实验系统提供的回收安全改进,例如LPD;并确定应用这些模拟器以支持海上测试动态接口的可行性。在两个中心实施的方法,具有良好的性能和与甲板运动的明显静止窗口相关性。描述了理论方法。结果在逐步困难的条件下在恢复的瞬间施加直升机时呈现出稳定性问题。摘要包括各种直升机恢复助剂的开发,仿真和测试,在模拟器测试期间应用。报告了瞬时自由度和加速度的测量,并进行了初步比较,以及之间,辅助发射和恢复和非辅助演变。讨论了船舶运动仿真和能源指标计划的理论和计算的简要概述。当操作员使用能量指数以发出恢复顶部时,空气车辆和甲板可用性远远超出所示的信封。如报告中所开发的,即使在海上条件最严重的情况下也会识别绿色甲板。期间可能是快速的,而是由于上升时间,甲板被延迟时段受到从绿色到红色的约束。

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