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Developing Flight Test Techniques to Ensure Proper Rigging of Highly Augmented Aircraft

机译:开发飞行测试技术以确保高架飞机的正确吊装

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Uncommanded rolling moments have been considered a natural part of the aging process of some F/A-18 airplanes. These rolling moments can range from an annoyance requiring constant trimming to a serious degradation in handling qualities, which can cause departures during maneuvering flight. Uncommanded rolling moments in flight can generally be eliminated with rigging if the surface that is causing the roll is known. Due to the highly augmented flight control architecture of the F/A-18, it is very difficult to isolate the actual control surface that is causing the Uncommanded rolling moment since so many surfaces contribute to roll control. NAWC-AD has developed techniques to identify the flight control surface causing uncom-manded rolling moments. These techniques have been used successfully on four F/A-18 airplanes to identify which flight control surface was causing uncommanded roll rates. Additional flight tests are planned to further refine the techniques described in this paper. These techniques have been demonstrated to reduce uncommanded rolling moments in the F/A-18 and can be applied to all aircraft.
机译:在某些F / A-18飞机的老化过程中,无规律的侧倾力矩已被视为自然的一部分。这些侧倾力矩的范围从需要不断调整的烦恼到操纵质量的严重下降,这可能会在机动飞行过程中造成偏离。如果知道引起滚动的表面,通常可以通过索具消除飞行中不受指令的滚动力矩。由于F / A-18的飞行控制架构高度增强,因此很难隔离导致无指令侧倾力矩的实际控制面,因为如此多的表面有助于侧倾控制。 NAWC-AD已经开发出识别飞控表面的技术,这些飞控表面会引起无用的侧倾力矩。这些技术已成功用于四架F / A-18飞机上,以识别哪个飞行控制面导致了不受控的侧倾率。计划进行额外的飞行测试,以进一步完善本文所述的技术。这些技术已被证明可以减少F / A-18的非指令性滚动力矩,并且可以应用于所有飞机。

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