An acceleration measurements-based approach for helicopter nonlinear flight control using Incremental Nonlinear Dynamic Inversion

Research output: Contribution to journal › Article › Scientific › peer-review

Original language	English
Pages (from-to)	1065-1077
Number of pages	13
Journal	Control Engineering Practice
Volume	21
Issue number	8
Publication status	Published - 2013

Keywords

@article{42262f1fb232447ba4a2af2c4f277436,

title = "An acceleration measurements-based approach for helicopter nonlinear flight control using Incremental Nonlinear Dynamic Inversion",

keywords = "CWTS 0.75 <= JFIS < 2.00",

author = "P Simplicio and MD Pavel and {van Kampen}, E and QP Chu",

year = "2013",

language = "English",

volume = "21",

pages = "1065--1077",

journal = "Control Engineering Practice",

issn = "0967-0661",

publisher = "Elsevier",

number = "8",

}

TY - JOUR

T1 - An acceleration measurements-based approach for helicopter nonlinear flight control using Incremental Nonlinear Dynamic Inversion

AU - Simplicio, P

AU - Pavel, MD

AU - van Kampen, E

AU - Chu, QP

PY - 2013

Y1 - 2013

KW - CWTS 0.75 <= JFIS < 2.00

M3 - Article

SN - 0967-0661

VL - 21

SP - 1065

EP - 1077

JO - Control Engineering Practice

JF - Control Engineering Practice

IS - 8

ER -