Ability to hover at fixed point in space is achieved accurately only with great deal of pilot effort because four integrations occur between pilot's input and resulting displacement of aircraft; by means of feedback proportional to helicopter's translation and its derivatives, hover augmentation system (HAS) reduces pilot effort; implementation of HAS is achieved by use of automatic pilot sensors and special computer to perform axis conversion from aircraft-axis system to earth-reference system; results of verification studies.
Hover augmentation system for helicopters
J Aircraft
Journal of Aircraft ; 4 , n 4
1967
7 pages
Article (Journal)
English
© Metadata Copyright Elsevier B. V. All rights reserved.
A hover augmentation system for helicopters.
AIAA | 1967
|A HOVER AUGMENTATION SYSTEM FOR HELICOPTERS
AIAA | 1966
|AERODYNAMIC INTERACTIONS ON AIRBUS HELICOPTERS' COMPOUND HELICOPTER RACER IN HOVER
British Library Conference Proceedings | 2020
|An L~1-Adaptive Vertical Speed Controller for Helicopters in Hover
British Library Conference Proceedings | 2015
|