Takeoff and landing control using force sensor by electrically-powered helicopters

Akira Shimada; Masanori Fujita

doi:10.1109/AMC.2006.1631633

Takeoff and landing control using force sensor by electrically-powered helicopters

Akira Shimada, Masanori Fujita

Research output: Contribution to conference › Paper › peer-review

8 Citations (Scopus)

Abstract

A takeoff and landing control of helicopters using a force sensor helicopter is introduced. The system consists of a small electrically-powered helicopter, a flight base under which the focre sensor is set, and a helicopter control terminal which is connected to a system controller. When the helicopter stands on the base, the force sensor outputs data corresponding to the weight of the helicopter. As the operational voltage rises, the helicopter almost take off from the base. Concurrently, the forse sensor output closes to 0. It means that lift force related to force output becomes from 0 N to the value cprresponding to the weight. This paper introduces the design process including system modeling and the experimental results.

Original language	English
Pages	62-65
Number of pages	4
DOIs	https://doi.org/10.1109/AMC.2006.1631633
Publication status	Published - 2006 Nov 21
Event	9th IEEE International Workshop on Advanced Motion Control, 2006 - Istanbul, Turkey Duration: 2006 Mar 27 → 2006 Mar 29

Conference

Conference	9th IEEE International Workshop on Advanced Motion Control, 2006
Country	Turkey
City	Istanbul
Period	06/3/27 → 06/3/29

ASJC Scopus subject areas

Control and Systems Engineering
Modelling and Simulation
Computer Science Applications
Electrical and Electronic Engineering

Access to Document

10.1109/AMC.2006.1631633

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abstract = "A takeoff and landing control of helicopters using a force sensor helicopter is introduced. The system consists of a small electrically-powered helicopter, a flight base under which the focre sensor is set, and a helicopter control terminal which is connected to a system controller. When the helicopter stands on the base, the force sensor outputs data corresponding to the weight of the helicopter. As the operational voltage rises, the helicopter almost take off from the base. Concurrently, the forse sensor output closes to 0. It means that lift force related to force output becomes from 0 N to the value cprresponding to the weight. This paper introduces the design process including system modeling and the experimental results.",

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AB - A takeoff and landing control of helicopters using a force sensor helicopter is introduced. The system consists of a small electrically-powered helicopter, a flight base under which the focre sensor is set, and a helicopter control terminal which is connected to a system controller. When the helicopter stands on the base, the force sensor outputs data corresponding to the weight of the helicopter. As the operational voltage rises, the helicopter almost take off from the base. Concurrently, the forse sensor output closes to 0. It means that lift force related to force output becomes from 0 N to the value cprresponding to the weight. This paper introduces the design process including system modeling and the experimental results.

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