This paper describes the initial development and validation of a flight simulation model of a Rotorsport UK Ltd. MT-03 autogyro. The model features rigid blades with a teetering rotor joint, which has wake interference effects modelled on the vertical surfaces of the vehicle. The initial model has been tuned to give a reasonable match of trim attitude and dynamic responses in each axis when compared with flight test data obtained from a brief campaign conducted specifically for this purpose. Rotor head mast angles are not particularly well predicted by the model but it is postulated, and some evidence provided, that inclusion of main rotor interference effects on the fuselage model would improve the fit, particularly for the mast roll angle. It was found that changing the main rotor inflow model from (Peters/He) three- to six-state improved the fidelity of the model’s main rotor speed and teeter angle at very low speeds. Continuing developments with the model and its validation are discussed.
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机译：本文介绍了Royorsport UK Ltd.Mt-03 Autogyro的飞行仿真模型的初步开发和验证。该模型具有刚性刀片，其具有夹持转子接头，其具有在车辆的垂直表面上建模的唤醒干扰效果。与从专门为此目的专门进行的简短运动获得的飞行测试数据相比，初始模型被调整为提供各种轴中的修剪姿态和动态响应。转子头部桅杆角度没有特别好的模型预测，但它被假设，并且提供了一些证据，其中包含主转子干扰对机身模型的影响将改善拟合，特别是对于桅杆辊角度。发现从（Peters / HE）的三到六个状态改变主转子流入模型改善了模型的主要转子速度和跷跷板角度的保真度。讨论了模型及其验证的持续发展。
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