Fighter Aircraft Closed Loop Handling Quality Simulation on Lateral-Directional Modes

Hindawan Hariowibowo, O. Arifianto, H. M. Pasaribu, H. Muhammad
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Abstract

In the early stage of fighter aircraft development, handling quality (HQ) become an important aspect in evaluating design results. One aspect of handling quality which involving pilot-in-the-loop, known as closed loop handling quality (CLHQ) will determine aircraft acceptability to fulfill its operational requirements. This paper explains the dynamic model of fighter aircraft for lateral-directional motions and simulate the CLHQ. The dynamic model consists of aircraft equation of motion and flight control system. In order to make CLHQ simulation, a pilot model has been added to the dynamic model. The simulation results are utilized to evaluate the sensitivity of the parameter values inside the elements of the dynamic model and the pilot model. Also, the current simulation results of CLHQ will be used for an evaluation of aircraft Pilot-Induced-Oscillation (PIO) phenomenon.
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战斗机横向模式闭环操纵质量仿真
在战斗机研制初期,操纵质量成为评价设计成果的一个重要方面。操纵质量的一个方面是闭环操纵质量(CLHQ),它涉及到飞行员在环,它将决定飞机的可接受性,以满足其操作要求。本文阐述了战斗机横向运动的动力学模型,并对其进行了仿真。动力学模型由飞行器运动方程和飞行控制系统组成。为了进行CLHQ仿真,在动态模型的基础上增加了先导模型。利用仿真结果评价了动态模型和先导模型各元素内部参数值的灵敏度。此外,CLHQ的当前仿真结果将用于评估飞机驾驶员诱导振荡(PIO)现象。
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