Development of UH-72A Simulator Model in Support of ADS-33 Training

W. Geyer, Barbara Gordon, C. Mattei, Dwight Robinson
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Abstract

The U.S. Naval Test Pilot School (USNTPS) qualifies engineering test pilots and flight test engineers for the Department of Defense (DoD) and foreign militaries. The school operates UH-72A and UH-60L aircraft as core rotary wing platforms used for airborne instruction in performance, flying qualities (FQ) and advanced flight control systems flight testing. The stability and control portion of the syllabus teaches both time and frequency domain flight test techniques in the evaluation of aircraft handling qualities (HQ); however, only classic time domain techniques have been instructed in the aircraft to support the curriculum. As frequency domain testing has become common practice across the DoD and within industry, the importance of providing entry level instruction in those flight test techniques cannot be overstated. Having students conduct many of the frequency domain test techniques in the aircraft is not practical. Providing adequate control measures such as real-time data monitoring and instructor pilot involvement on each flight to ensure safe execution would place an unrealistic burden on the USNTPS staff and adversely impact the airworthiness of the school’s aircraft. The USNTPS simulation laboratory recently received a high fidelity UH-60 flight dynamics simulation model enabling the instruction of frequency domain flight test techniques and the collection of predictive HQ data as defined within the ADS-33E-PRF, Handling Qualities Requirements for Military Rotorcraft. These data are used to support assigned HQ flights flown on Naval Test Wing Atlantic’s ADS-33 Mission Task Element course. Conducting systems identification testing and the subsequent development of a high fidelity UH-72A flight dynamics simulation model allows the execution of the entire Low Airspeed FQ exercise across both core platforms. Simulator-based predictive HQ data are now utilized in support of assigned HQ flights in the respective aircraft. This paper covers the development of the UH-72A simulation model, flight test efforts supporting that development and the successful integration of the model as a means to collect predictive HQ data in support of the Low Airspeed FQ exercise at the USNTPS.
支持ADS-33训练的UH-72A模拟器模型的开发
美国海军试飞员学校(USNTPS)为国防部(DoD)和外国军队提供工程试飞员和飞行测试工程师资格。学校运营UH-72A和UH-60L飞机作为核心旋翼平台,用于性能、飞行质量(FQ)和先进飞行控制系统飞行测试的机载教学。稳定性和控制部分的教学大纲教时域和频域飞行测试技术在飞机处理质量(HQ)的评估;然而,只有经典的时域技术已指示在飞机上,以支持课程。由于频域测试已经成为国防部和工业界的普遍做法,在这些飞行测试技术中提供入门级指导的重要性不能被夸大。让学生在飞机上进行许多频域测试技术是不实际的。提供足够的控制措施,如实时数据监控和指导飞行员参与每次飞行,以确保安全执行,将给USNTPS工作人员带来不切实际的负担,并对学校飞机的适航性产生不利影响。USNTPS仿真实验室最近收到了一个高保真的UH-60飞行动力学仿真模型,该模型能够指导频域飞行测试技术,并收集ADS-33E-PRF中定义的预测HQ数据,军用旋翼机处理质量要求。这些数据用于支持在海军大西洋测试联队ADS-33任务单元课程上飞行的指定总部飞行。进行系统识别测试和高保真UH-72A飞行动力学仿真模型的后续开发,允许在两个核心平台上执行整个低空速FQ演习。基于模拟器的预测总部数据现在被用于支持各自飞机上指定的总部飞行。本文涵盖了UH-72A仿真模型的开发,支持该开发的飞行测试工作以及该模型的成功集成,作为收集预测HQ数据的一种手段,以支持USNTPS的低空速FQ演习。
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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