Real-time flight control design for a spherical blimp

A. Rojas-Moreno, F. Santos–Rodriguez, Noel Curinaupa–Cespedes
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引用次数: 1

Abstract

This paper develops a real-time software written in LabVIEW code to test a novel flight control strategy for a spherical blimp. Such a blimp will have an spherical hull filled with helium. Four tetrahedrally-arranged driving units (DU) were designed and constructed, with each DU having a thruster with propeller with the ability to rotate, due to the action of a DC servomotor. Such DU will be mounted on the blimp for locomotion. The mechanical design is aimed to make the blimp near NBP (Neutral Buoyancy Position). Starting from any NBP, the proposed flight logic strategy permits the blimp to move in any direction: up, down, right, left, forward and backward.
球形飞艇的实时飞行控制设计
本文开发了一个用LabVIEW代码编写的实时软件,以测试一种新的球形飞艇飞行控制策略。这种飞艇将有一个充满氦气的球形外壳。设计并构建了四个四面体排列的驱动单元(DU),每个DU都有一个推进器,由于直流伺服电机的作用,具有旋转能力。这样的DU将被安装在飞艇上以供移动。机械设计的目的是使飞艇接近NBP(中性浮力位置)。从任何NBP开始,提出的飞行逻辑策略允许飞艇在任何方向上移动:上、下、右、左、前、后。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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