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Experiment platform for pan-tilt control of a small scale autonomous helicopter

机译:小型自主直升机的云台控制实验平台

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To analyze the characteristic of an onboard pan-tilt control system to enable an unmanned aerial vehicle (UAV) to Track a ground target, and to verify the stability of the tracking controller and to test the performance of the controller, an experiment platform for pan-tilt control of a small scale autonomous helicopter is designed and then implemented. The system consists of four components including the model of the helicopter, pan-tilt camera, onboard equipment and ground control center. Moreover, the control software is developed by using C++ based on the Visual Studio environment, where multi-threading technique is adopted to make the modules independent of each other. The system not only reliably reflects the dynamics of a practical pan-tilt control system of a small scale autonomous helicopter, but also provides friendly user interface which brings much convenience to implemented and then tested various control strategies. Finally, all the function modules are tested in the ground and air condition respectively, and the obtained experiment results demonstrates the reliability of the system.
机译:为了分析机载云台控制系统的特性,以使无人飞行器(UAV)能够跟踪地面目标,并验证跟踪控制器的稳定性并测试控制器的性能,这是一种用于平移的实验平台设计并实现了小型自主直升机的倾斜控制。该系统由四个部分组成,包括直升机模型,云台摄像机,机载设备和地面控制中心。此外,控制软件是使用基于Visual Studio环境的C ++开发的,其中采用多线程技术使模块彼此独立。该系统不仅可靠地反映了小型自主直升机的实际云台控制系统的动态,而且还提供了友好的用户界面,为实施和测试各种控制策略带来了极大的便利。最后,对所有功能模块分别在地面和空调条件下进行了测试,获得的实验结果证明了系统的可靠性。

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