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首页> 外文期刊>Journal of Intelligent & Robotic Systems: Theory & Application >Concepts and Validation of a Small-Scale Rotorcraft Proportional Integral Derivative (PID) Controller in a Unique Simulation Environment
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Concepts and Validation of a Small-Scale Rotorcraft Proportional Integral Derivative (PID) Controller in a Unique Simulation Environment

机译：独特仿真环境中小型旋翼飞机比例积分微分（PID）控制器的概念和验证

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摘要

At the current time, the U.S. Army Research Laboratory's (ARL's) Vehicle Technology Directorate is interested in expanding its Unmanned Vehicles Division to include rotary wing and micro-systems control. The intent is to research unmanned aircraft systems not only for reconnaissance missions but also for targeting and lethal attacks. This project documents ongoing work expanding ARL's program in research and simulation of autonomous control systems. A proportional integral derivative control algorithm was modeled in Simulink (Simulink is a trademark of The MathWorks) and communicates to a flight simulator modeling a physical radio-controlled helicopter. Waypoint navigation and flight envelope testing were then systematically evaluated to the final goal of a feasible autopilot design. Conclusions are made on how to perhaps make this environment more dynamic in the future.
机译：目前，美国陆军研究实验室（ARL）的车辆技术总局有意将其无人飞行器部门扩大到包括旋翼和微系统控制。目的是研究无人飞机系统，不仅用于侦察任务，还用于瞄准和致命攻击。该项目记录了正在进行的工作，正在扩展ARL在自主控制系统的研究和仿真中的计划。比例积分微分控制算法在Simulink中建模（Simulink是The MathWorks的商标），并与模拟物理无线电控制直升机的飞行模拟器通信。然后，系统地评估了航点导航和飞行包线测试，以达到可行的自动驾驶仪设计的最终目标。关于如何使将来的环境更加动态的结论。

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