Engine control design using compressor guided vanes during autorotation power recovery
type: Item
instance of: scholarly article
title: Engine control design using compressor guided vanes during autorotation power recovery
zbMATH Open document ID: 1390.93340
author: Fengyong Sun
author: Hai-Bo Zhang
published in: Arabian Journal for Science and Engineering
publication date: 2018-06-14T00:00:00Z
Mathematics Subject Classification ID: 93B55
Mathematics Subject Classification ID: 93B36
Mathematics Subject Classification ID: 94C05
zbMATH DE Number: 6888849
zbMATH Keywords: helicopter
zbMATH Keywords: engine
zbMATH Keywords: integrated model
zbMATH Keywords: autorotation
zbMATH Keywords: control
MaRDI profile type: Publication
full work available at URL: s13369-016-2336-7
OpenAlex ID: W2540692825
cites work: Robust Exact Pole Placement via an LMI-Based Algorithm
cites work: Analytical prediction of height-velocity diagram of a helicopter using optimal control theory
cites work: Robust full degree-of-freedom tracking control of a helicopter
cites work: H/sub ∞/ design with pole placement constraints: an LMI approach
cites work: Q4003793
DOI: 10.1007/S13369-016-2336-7
description: scientific article; zbMATH DE number 6888849