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Designing 3-DOF Hardware-In-The-Loop Test Platform Controlling Multirotor Vehicles

机译:设计用于控制多旋翼飞行器的3-DOF硬件在环测试平台

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Main idea of this paper is the development of Hardware-in-the-Loop test platform in order to flight mechanical modeling and better stabilization of multirotor vehicles via different feedback control structures, including PID controllers. First, nonlinear mathematical model of the quadrotor platform is built and validated via Matlab/Simulink based simulation environment.Then, Hardware-in-the-Loop (HIL) test scenario is developed to analyze and tune controller parameters with the help of in-house designed testbed mechanism. Next step is observing the quadrotor attitude maneuvers via embedded hardware over the gyroscopic gimballed testbed. The HIL testbed enables us validate and calibrate model and control parameters within real-time environment including inertial and mechanical sensors for multirotor systems. In this study, the particular platform is IRIS cross-type quadrotor vehicle PID based control for stable hover flight.
机译:本文的主要思想是开发硬件在环测试平台,以通过不同的反馈控制结构(包括PID控制器)对多旋翼飞行器进行飞行机械建模和更好的稳定性。首先,通过基于Matlab / Simulink的仿真环境构建并验证了四旋翼平台的非线性数学模型,然后开发了硬件在环(HIL)测试方案,以在内部帮助下分析和调整控制器参数设计的测试平台机制。下一步是通过陀螺仪万向试验台上的嵌入式硬件观察四旋翼姿态操纵。 HIL测试平台使我们能够在实时环境中验证和校准模型和控制参数,包括用于多转子系统的惯性和机械传感器。在这项研究中,特定的平台是基于IRIS十字型四旋翼飞行器PID的控制,用于稳定的悬停飞行。

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