scholarly journals Helicopter Control During Landing on a Moving Confined Platform

IEEE Access ◽  
2020 ◽  
Vol 8 ◽  
pp. 107315-107325 ◽  
Author(s):  
Sebastian Topczewski ◽  
Janusz Narkiewicz ◽  
Przemyslaw Bibik
Keyword(s):  
Helicopter Control

A Parallel Fly-by-Wire Helicopter Control System.

1982 ◽  
Author(s):  
M. R. Murphy ◽  
D. E. Haskins
Keyword(s):  
Control System ◽  
Helicopter Control

A 2-DoF Haptic Support System for Helicopter Control Tasks based on Pilot Intent Estimation

2019 ◽  
Author(s):  
Giulia D'Intino ◽  
Mario Olivari ◽  
Stefano Geluardi ◽  
Lorenzo Pollini ◽  
Heinrich Bülthoff
Keyword(s):  
Support System ◽  
Helicopter Control

Investigation of Airfoil Dynamic Stall and Its Influence on Helicopter Control Loads

1972 ◽  
Author(s):  
Franklin O. Carta ◽  
Gerald L. Commerford ◽  
Raymond G. Carlson ◽  
Robert H. Blackwell
Keyword(s):  
Dynamic Stall ◽  
Helicopter Control

Analysis of combined passively and actively morphing blade root chord length and blade taper for helicopter control

2019 ◽  
Vol 92 (2) ◽  
pp. 172-179
Author(s):  
Firat Sal
Keyword(s):  
Flight Control ◽  
Chord Length ◽  
Flight Control System ◽  
Control Effort ◽  
Simultaneous Application ◽  
Content Type ◽  
Helicopter Control ◽  
Helicopter Blade ◽  
Blade Root ◽  
Autonomous Helicopter

Purpose The purpose of this study is to examine the effect of passive and active morphing of blade root chord length and blade taper on the control effort of the flight control system (FCS) of a helicopter. Design/methodology/approach Physics-based helicopter models, which are functions of passive and active morphing, are created and applied in helicopter FCS design to determine the control effort. Findings Helicopters, having both passively and actively morphing blade root chord length and blade taper, experience less control effort than the ones having either only passively morphing blade root chord length or only blade taper or only actively morphing blade root chord length and blade taper. Practical implications Both passively and actively morphing blade root chord length and blade taper can be implemented for more economical autonomous helicopter flights. Originality/value Main novelty of our article is simultaneous application of passive and active morphing ideas on helicopter root chord length and blade taper. It is also proved in this study that using both passive and active morphing ideas on helicopter blade root chord and blade taper causes much less energy consumption than using either only passive morphing idea on helicopter blade root chord and blade taper or only active morphing idea on helicopter blade root chord and blade taper. This also reduces fuel consumption and also makes environment cleaner.

Helicopter Control Systems: A History

2003 ◽  
Vol 26 (1) ◽  
pp. 12-18 ◽  
Author(s):  
Raymond W. Prouty ◽  
H. C. Curtiss
Keyword(s):  
Control Systems ◽  
Helicopter Control
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