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AUTONOMOUS FLIGHT CONTROL DEVICE AND SMALL-SIZE UNMANNED HELICOPTER WITH DEVICE

机译:自主飞行控制装置和带有装置的小型无人驾驶直升机

摘要

PROBLEM TO BE SOLVED: To provide an autonomous flight control device manufactured on the basis of a linear model and downsized, which stably controls a small-size unmanned helicopter to be taken off or landed.;SOLUTION: The autonomous flight control device 100 comprises; a vertical direction control part 110 having a vertical speed control part 112 for calculating a vertical speed control value on the basis of a current vertical speed and a predetermined vertical speed target value to be used in takeoff control or landing control; and a horizontal direction control part 120 having a horizontal speed control part 122 for calculating a horizontal speed control value on the basis of a current horizontal speed and a predetermined horizontal speed target value, and an attitude angle control part 123 for calculating an attitude angle control value on the basis of a current attitude angle and a horizontal speed control value. The vertical speed control value calculated by the vertical speed control part 112 is outputted as a vertical direction control value, and the attitude angle control value calculated by the attitude angle control part 123 is outputted as a horizontal direction control value.;COPYRIGHT: (C)2008,JPO&INPIT
机译:解决的问题:提供一种基于线性模型制造并减小尺寸的自动飞行控制装置,其稳定地控制小型无人直升机的起飞或降落。解决方案:自动飞行控制装置100包括:垂直方向控制部110,具有垂直速度控制部112,该垂直速度控制部112用于基于当前的垂直速度和预定的垂直速度目标值来计算垂直速度控制值,以用于起飞控制或着陆控制。水平方向控制部分120具有水平速度控制部分122,用于基于当前水平速度和预定水平速度目标值来计算水平速度控制值;以及姿态角控制部分123,用于计算姿态角控制该值基于当前姿态角和水平速度控制值。由垂直速度控制部112计算出的垂直速度控制值作为垂直方向控制值输出,由姿态角控制部123计算出的姿态角控制值作为水平方向控制值输出。 )2008,日本特许厅

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