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首页> 外文会议>International conference on computer design and applications >The Design and Simulation of Low-Cost and Super-Applicability Flight Control System of Super-Size Uav
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The Design and Simulation of Low-Cost and Super-Applicability Flight Control System of Super-Size Uav

机译：超大型无人机低成本超适用飞控系统的设计与仿真

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In this paper, considering the stability and robustness of the aircraft, the flight control system is designed following the aspect of high flexibility and low cost. Comparing with the flight control system of super-size high-subsonic Unmanned Aerial Vehicle (UAV) in the world, the system presented in this paper has adopted the inimitable control technique of flying-off course low-cost combinatorial navigation strategy and the advanced safety scheme, which can guarantee the performance, degrade the cost and extend the airspace and groundspace of the aircraft.Through quite a few simulations, the results show that this system can guarantee the attitude and altitude stable. The error between the flight path and programming path is very small. Flight curve is prefect; and the system performances can be achieved completely.
机译：考虑到飞机的稳定性和鲁棒性，本文从高灵活性和低成本的角度设计了飞行控制系统。与世界上超大型超音速无人机的飞行控制系统相比，本文提出的系统采用了飞行路线低成本组合导航策略的独特控制技术和先进的安全性。通过大量的仿真实验，结果表明该系统可以保证飞机的姿态和高度稳定。飞行路径和编程路径之间的误差非常小。飞行曲线完美无缺;系统性能可以完全实现。

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