Modeling and simulation of longitudinal autopilot for general aviation aircraft

机译：通用航空飞机纵向自动驾驶仪的建模与仿真

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From the dawn of advanced aerospace technology, the aspect of stability and automated control is an important field of research interest providing ease of handling and friendly assistance for piloting. Considering this challenging aspect, development of automated control system is chosen for this research. The aim of this paper is to design a longitudinal autopilot for a general aviation aircraft and to analysis the performance of the developed model both for normal condition and atmospheric disturbance. To improve the overall performance, stability of the system and to overcome the atmospheric disturbance a compensator along with a PID controller has been designed. Simulation results of MATLAB Simulink have been also analyzed.

机译：从先进的航空航天技术诞生之日起，稳定性和自动控制便成为重要的研究领域，为驾驶员提供易于操作和友好的帮助。考虑到这一具有挑战性的方面，本研究选择了自动控制系统的开发。本文的目的是为通用航空飞机设计纵向自动驾驶仪，并分析所开发模型在正常状态和大气干扰下的性能。为了提高整体性能，系统稳定性并克服大气干扰，已设计了补偿器和PID控制器。还对MATLAB Simulink的仿真结果进行了分析。

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来源
《2016 5th International Conference on Informatics, Electronics and Vision》|2016年|490-495|共6页
会议地点 Dhaka(BD)
作者
Md. Tanjemul Islam; Md. Shah Alam; Md. Ashiqur Rahman Laskar; Atul Garg;
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作者单位

Department of Aeronautical Engineering, Military Institute of Science and Technology (MIST), Dhaka, Bangladesh;

Department of Aeronautical Engineering, Military Institute of Science and Technology (MIST), Dhaka, Bangladesh;

Department of Aeronautical Engineering, Military Institute of Science and Technology (MIST), Dhaka, Bangladesh;

Department of Aeronautical Engineering, Military Institute of Science and Technology (MIST), Dhaka, Bangladesh;

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原文格式 PDF
正文语种 eng
中图分类
关键词
Aircraft; Atmospheric modeling; Mathematical model; Aerospace control; MATLAB; Elevators;

机译：飞机;大气建模;数学模型;航空航天控制; MATLAB;电梯;

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专利

1. Improved disturbance rejection control based on H_∞ synthesis and equivalentinput-disturbance for aircraft longitudinal autopilot design [J] . Li Tong, Yang Huabo, Tian Jiayi, Proceedings of the Institution of Mechanical Engineers . 2019,第9期

机译：基于H_∞综合和等效输入扰动的改进的航空器纵向自动驾驶仪抗扰控制
2. Improved disturbance rejection control based on H_∞ synthesis and equivalentinput-disturbance for aircraft longitudinal autopilot design [J] . Li Tong, Yang Huabo, Tian Jiayi, Proceedings of the Institution of Mechanical Engineers . 2019,第9期

机译：基于H_∞合成的改进的扰动抑制控制和飞机纵向自动驾驶仪设计的同等施用扰动
3. Aircraft Longitudinal Control without a Pitch Command in the Autopilot [J] . L. G. Romanenko, A. G. Romanenko, G. G. Samarova Russian Aeronautics . 2014,第4期

机译：自动驾驶仪中没有俯仰命令的飞机纵向控制
4. Modeling and simulation of longitudinal autopilot for general aviation aircraft [C] . Md. Tanjemul Islam, Md. Shah Alam, Md. Ashiqur Rahman Laskar, International Conference on Informatics, Electronics and Vision . 2016

机译：通用航空飞机纵向自动驾驶仪的建模与仿真
5. Effect of the autopilot on pilot performance during ils approaches in general aviation technically advanced aircraft. [D] . Geske, Robert C. 2013

机译：在通用航空技术先进的飞机上，自动驾驶对进近过程中飞行员性能的影响。
6. Progressive Damage Numerical Modelling and Simulation of Aircraft Composite Bolted Joints Bearing Response [O] . Guoqiang Gao, Luling An, Ioannis K. Giannopoulos, 2020

机译：飞机复合螺栓接头轴承响应的渐进损伤数值建模与仿真
7. Design for Simulation System of the Aviation Autopilot [O] . Yinsai Guo, Yi Zhang, Mingke Cheng, 2015

机译：航空自动驾驶仪仿真系统设计
8. Design, implementation and flight testing of PIF autopilots for general aviation aircraft [R] . Broussard, J. R. 1983

机译：通用航空飞机pIF自动驾驶仪的设计，实施和飞行试验

Modeling and simulation of longitudinal autopilot for general aviation aircraft

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