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Autonomous control method for small unmanned helicopter

机译:小型无人直升机的自主控制方法

摘要

An autonomous control method autonomously controls a small unmanned helicopter toward target values, such as a set position and velocity, by deriving model formulas well suited for the autonomous control of small unmanned helicopters, by designing an autonomous control algorithm based on the model formulas, and by calculating the autonomous control algorithm. The autonomous control system includes sensors that detect current position, attitude angle, altitude relative to the ground, and absolute azimuth of a nose of the small unmanned helicopter; a primary computational unit that calculates optimal control reference values for driving the helicopter from a target position or velocity values; a secondary computational unit that converts data collected by the sensors and the computational results as numeric values that are output by the primary computational unit into pulse signals; a ground station host computer used as the computational unit for the autonomous control system; and so on.
机译:一种自主控制方法,通过推导非常适合小型无人直升机的自主控制的模型公式,并基于模型公式设计一种自主控制算法,从而自动地将其控制在诸如设定位置和速度等目标值上。通过计算自主控制算法。自主控制系统包括传感器,该传感器检测小型无人机的当前位置,姿态角,相对于地面的高度以及机鼻的绝对方位角;主计算单元,其从目标位置或速度值计算用于驱动直升机的最佳控制参考值;次级计算单元,其将传感器收集的数据和计算结果作为由初级计算单元输出的数值转换为脉冲信号;地面站主计算机,用作自主控制系统的计算单元;等等。

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