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首页> 外文会议>International Symposium on Unmanned Aerial Vehicles >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：小型旋翼飞机比例积分导数（PID）控制器在独特的仿真环境中的概念和验证

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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 Math Works) 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：在当前，美国陆军研究实验室（ARL）的车辆技术局有兴趣扩大其无人驾驶车辆部门，包括旋翼和微系统控制。目的是为了研究无人机的飞机系统，不仅适用于侦察任务，而且还用于瞄准和致命的攻击。该项目宣布持续工作扩展ARL的自主控制系统的研究和仿真方案。在Simulink中建模了比例积分衍生衍生物控制算法（Simulink是数学作品的商标），并传达到用于模拟物理无线电控制直升机的飞行模拟器。然后系统地评估WayPoint导航和飞行信封测试以获得可行的自动驾驶仪设计的最终目标。结论是关于如何使这一环境在未来更加活跃。

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