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首页> 外文期刊>IEEE Aerospace and Electronic Systems Magazine >Low complexity, low-cost, altitude/heading hold flight control system
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Low complexity, low-cost, altitude/heading hold flight control system

机译：低复杂性，低成本，高度/标题持有飞行控制系统

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摘要

For many one-way unmanned aerial vehicle payload delivery and remote sensing missions, the heading to the target location and local winds are known. For these missions, only altitude and heading hold features are needed. Further, because the vehicle will not be returning, minimizing cost is a priority. Due to the desire to reduce the physical size of the vehicle, the flight control system needs to be of minimal complexity to facilitate miniaturization. Presented is a prototype altitude/heading hold flight control system that has been developed for use in small, stable UAV platforms. Topics covered in this paper include system architecture, hardware, user interface, and preliminary test-flight results. A brief description of the miniature target aircraft, the Naval Research Laboratory's Micro Tactical Expendable (MITE), will be presented as a representation of the class of vehicle under consideration.
机译：对于许多单向无人的空中车辆有效载荷传递和遥感任务，已知前往目标位置和局部风。对于这些任务，只需要高度和标题持有功能。此外，因为车辆不会返回，最小化成本是优先级。由于渴望减少车辆的物理尺寸，飞行控制系统需要具有最小的复杂性，以便于小型化。呈现是一个原型高度/标题持有飞行控制系统，该控制系统已经开发用于小型稳定的UAV平台。本文涵盖的主题包括系统架构，硬件，用户界面和初步测试飞行结果。缩小目标飞机的简要描述，海军研究实验室的微型战术消耗（螨）将作为正在考虑的车辆类的代表提出。

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