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B-2 Flight control system development flight test lessons learned

机译:B-2飞行控制系统开发飞行测试经验教训

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The B-2 aircraft completed Engineering and Manufacturing Development (EMD) flitht test in June 1997.This marked the end to a highly successful program where many challenges were overcome to produce a revolutionary combat capable aircraft.The unique flying wing configuration,large airspeed and altitude envelope,and emphasis on low observability presented the flight control development team with a formidable task.The goal of B-2 Flight Control System (FCS) development was to provide an aircraft with satisfactory handling qualities during all phases of flight,for all vehicle configurations,and under a wide range of atmospheric conditions.Meeting this goal required integration of the flight control,aerodynamic,structural,propulsion,subsystem,and avionics disciplines.This integrated approach was used in the flight test program provides a technical overview of selected unique B-2 aircraft characteristics and FCS design challenges encountered.Flight test results,anomalies encountered.solutions implemented,and test management techniques will also be discussed.the methods outlined and lessons learned may be useful for testing current and future aircraft.
机译:B-2飞机于1997年6月完成了工程和制造开发(EMD)氟三丝试验。这标志着一项高度成功的计划,克服了许多挑战,以生产一架革命性的作战飞机。独特的飞行机翼配置,宽敞的飞机和高度信封,并强调低可观测性,具有强大的任务。B-2飞行控制系统(FCS)开发的目标是为所有车辆的所有阶段提供令人满意的处理质量的飞机配置,并且在各种大气条件下。此目标需要集成飞行控制,空气动力学,结构,推进,子系统和航空电子学科。在飞行试验计划中使用了综合方法,提供了所选独特的技术概述B-2飞机特性和FCS设计挑战遇到。风光测试结果,异常遇到。实施的实施,也将讨论测试管理技术。所概述的方法和课程的课程对于测试当前和未来的飞机可能是有用的。

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