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首页> 外文会议>Congress of the International Council of the Aeronautical Sciences;ICAS 2008 >CESSNA CITATION CJ1 FLIGHT-TEST DATA GATHERING AND LEVEL-C SIMULATOR MODEL DEVELOPMENT
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CESSNA CITATION CJ1 FLIGHT-TEST DATA GATHERING AND LEVEL-C SIMULATOR MODEL DEVELOPMENT

机译：CESSNA CITATION CJ1飞行测试数据汇总和LEV-C仿真器模型开发

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The National Research Council of Canada's Institute for Aerospace Research (NRC Aerospace) Flight Research Laboratory (FRL) was contracted by Mechtronix Systems Incorporated (MSI), Montreal, Canada, to conduct flight-test data gathering and simulator model development for the Cessna Citation CJ1 business aircraft. The data collected and the models developed conformed to the FAA Advisory Circular 120-40B Level C Airplane Simulator Qualification.NRC Aerospace created the complete simulator model from end-to-end; developing aerodynamic, engine performance, engine gauge, reversible flight control, and ground dynamics models following the collection of flight-test data. The engine performance modelling was unique since the novel NRC inflight propulsion identification technique (IPSI) was used to develop the model solely using flight data. Engine gauge, reversible flight control and ground dynamics models were added to the existing NRC aerodynamic modelling capability to form an enhanced simulation environment and were qualified to Level-C standards.This program has clearly demonstrated major improvements in modelling efficiency and a reduction in time to six months required to develop an end-to-end simulator mathematical model for a fixed wing aircraft using flight-test data.
机译：加拿大航空航天研究所（NRC航空航天）飞行研究实验室（FRL）的国家研究委员会由加拿大蒙特利尔的Mechtronix Systems Incorporated（MSI）承包，用于为Cessna Citation CJ1进行飞行测试数据收集和模拟器模型开发公务机。收集的数据和开发的模型均符合FAA咨询通告120-40B C级飞机模拟器的资格要求。 NRC航空航天从端到端创建了完整的仿真器模型;在收集飞行测试数据后，开发空气动力学，发动机性能，发动机规格，可逆飞行控制和地面动力学模型。发动机性能模型是独特的，因为仅使用飞行数据就使用了新颖的NRC机上推进识别技术（IPSI）来开发模型。发动机压力表，可逆飞行控制和地面动力学模型已添加到现有的NRC空气动力学建模功能中，以形成增强的仿真环境，并符合C级标准。 该程序清楚地证明了建模效率的重大提高，并且使用飞行测试数据为固定翼飞机开发了端到端模拟器数学模型所需的时间减少了六个月。

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