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Design, Development and Evaluation of Longitudinal Autopilot for An Unmanned Aerial Vehicle Using X-Plane/Simulink

机译:使用X平面/ Simulink对无人空中车辆纵向自动驾驶仪的设计,开发和评估

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Presently there is a vast interest in unmanned aerial vehicle (UAV) development given its civilian and military applications. One of the main UAV components is autopilot system. Its development invariably demands several lab simulations and field tests. Generally after an UAV crash few parts remain unused. Thus, before embedding an autopilot system, it has to be exhaustively lab tested. With educational and research purposes in autopilot control systems development area, a test platform is herein proposed. It employs Matlab/Simulink to run the autopilot controller under test. The autopilot controller designed on Matlab/ Simulink is tested by controlling an aircraft on X-Plane. The inputs given to the aircraft flight control surfaces in the X-Plane are simultaneously sent to the microcontroller which translates these commands into effective servo movement control. Through this platform, designed autopilot systems can be applied into models similar to real aircraft minimizing risks and increasing flexibility for design changes. As study case, tests results from a pitch attitude autopilot system are presented.
机译:目前,鉴于其平民和军事申请,对无人机(UAV)开发的巨大兴趣。其中一个主要的UAV组件是自动驾驶仪系统。其发展总是要求几个实验室模拟和现场测试。一般在UAV崩溃后,少数部分仍未使用。因此,在嵌入自动驾驶系统之前,它必须有详尽的实验室测试。在自动驾驶仪控制系统开发区的教育和研究目的,本文提出了一种测试平台。它采用MATLAB / SIMULINK运行被测自动驾驶仪控制器。通过控制X平面上的飞机测试在Matlab / Simulink上设计的自动驾驶仪控制器。给出给X平面中的飞机飞行控制表面的输入同时发送到微控制器,该微控制器将这些命令转换为有效的伺服运动控制。通过该平台,设计的自动驾驶仪系统可以应用于类似于真正的飞机的模型,从而最大限度地减少风险,并提高设计变化的灵活性。作为研究案例,介绍了音高姿态自动驾驶仪系统的测试。

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