Comparative Flight Test Evaluation of Passive and Active External Slung Load Dynamics

M. Alexander, E. Perron, Perry Comeau, David Rancourt
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Abstract

The National Research Council of Canada and Université de Sherbrooke performed flight testing of an Actively Stabilized Slung Load on the NRC Bell 206 Research Aircraft. Hover, Attitude Capture, NRC designed Lateral Precision Hover, and Frequency Sweep mission tasks were performed for Bare Airframe, Passive Water-Filled Barrel and Active Slung Load configurations. Load Mass Ratios of 0.12 with pendulum modes of 1.3 rad/sec were identified for both configurations. Time domain response indicated that both loads remained controllable under excitation by pilot gain, winds, and helicopter-load mode coalescence. Frequency domain analyses confirmed pilot comments indicating HQR-4 handling qualities ratings for bare airframe and stable load behaviors. This degraded to HQR-5 for task execution with load oscillation effects rated at pilot induced oscillation tendency of PIO/T-4. Barrel load HQR degradation related to load inertial and surface area drag effects versus active tether feedback and roll-pitch actuation disharmony of the Active load. Though not optimized, this load’s swing behavior (consistent period and rate) can aid in management of aircraft rate response and pilot compensation. Overall, comparable passive and active test results indicate potential for magneto-rheological actuation to improve slung load mission task performance.
被动和主动外挂载动力学比较飞行试验评价
加拿大国家研究委员会和舍布鲁克大学在NRC贝尔206研究飞机上进行了主动稳定悬挂载荷的飞行测试。悬停、姿态捕获、NRC设计的横向精确悬停和频率扫描任务在裸机身、被动充水桶和主动悬挂载荷配置下执行。载荷质量比为0.12,摆模为1.3 rad/sec。时域响应表明,在飞行员增益、风力和直升机-载荷模式合并的激励下,两种载荷都是可控的。频域分析证实了飞行员的评论,表明HQR-4在裸机身和稳定负载行为下的处理质量评级。在执行任务时,这一等级降为HQR-5,负载振荡效应达到PIO/T-4的先导诱导振荡趋势。桶载HQR退化与负载惯性和表面阻力效应以及主动系绳反馈和主动负载的滚转-俯仰驱动不协调有关。虽然没有优化,但这种负载的摆动行为(一致的周期和速率)可以帮助管理飞机的速率响应和飞行员补偿。总的来说,比较的被动和主动测试结果表明,磁流变驱动有可能改善悬挂载荷任务的性能。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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