Model-based manoeuvre analysis: a path to a new paradigm in aircraft flight dynamics

B. Shayak, Sarthak Girdhar, Sunandan Malviya
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Abstract

We propose a closed-form system of nonlinear equations for the pitch plane or longitudinal motions of a fixed-wing aircraft and use it to demonstrate a possible path to the unification of theoretical flight dynamics and practical analysis of aircraft manoeuvres. The derivation of an explicit model free of data tables and interpolated functions is enabled by our use of empirical formulae for lift and drag which agree with experiments. We validate the model by recovering the well-known short period and phugoid modes, and the regions of normal and reversed command. We then use the model to present detailed simulations of two acrobatic manoeuvres, an Immelmann turn and a vertical dive. Providing new quantitative insights into the dynamics of aviation, our model-based manoeuvre analysis has the potential to impact both the academic flight dynamics curriculum and the ground training program for pilots of manned and unmanned aircraft. Possible consequences of future model-centric pilot training may include improved safety standards in general and commercial aviation as well as expedited theoretical course completion in air transport.
基于模型的机动分析:通向飞机飞行动力学新范例的道路
我们提出了一个固定翼飞机俯仰平面或纵向运动的闭式非线性方程组,并用它来证明统一飞行动力学理论和飞机操纵实际分析的可能途径。通过使用与实验相符的升力和阻力经验公式,我们可以推导出一个不需要数据表和插值函数的显式模型。我们通过恢复众所周知的短周期和phugoid模式以及正常和反向指令区域来验证模型。然后,我们利用该模型对伊梅尔曼转弯和垂直俯冲这两种杂技动作进行了详细模拟。我们基于模型的机动分析为航空动力学提供了新的定量见解,有可能对飞行动力学学术课程以及有人驾驶飞机和无人驾驶飞机飞行员的地面培训计划产生影响。未来以模型为中心的飞行员培训可能带来的后果包括提高通用航空和商业航空的安全标准,以及加快航空运输理论课程的完成。
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