Development and flight-test verification of two-dimensional rotational low-airspeed sensor for small helicopters

Abstract This paper describes the development and the verification of flight test results of a differential pressure-based, two-dimensional low-airspeed sensor designed for the navigation or disturbance detection in small helicopters. The compact and lightweight sensor is integrated with the main ro...

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Bibliographic Details
Main Authors: Daigo Fujiwara, Takumi Tonoike
Format: Article
Language:English
Published: SpringerOpen 2024-04-01
Series:ROBOMECH Journal
Subjects:
Online Access:https://doi.org/10.1186/s40648-024-00274-2