Design of multi-mode flight control system for unmanned helicopter

Hongzhe Xu; Jun Huang; Yaoming Zhou

Design of multi-mode flight control system for unmanned helicopter

Hongzhe Xu^*
, Jun Huang
, Yaoming Zhou

^*Corresponding author for this work

School of Aeronautic Science and Engineering

Beihang University

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

3 Scopus citations

Abstract

Based on the special requirements of flight control and navigation system of unmanned helicopter, this paper present the main framework of flight control system in a certain type of unmanned helicopter, proposed three flight control modes based on different design stages, gave the autonomous control algorithm and the smoothing method while switching between remote control mode and stability augmentation mode, ultimately proved the feasibility of flight control and navigation program through the semi-physical simulation test and flight test.

Original language	English
Title of host publication	Proceedings of the 30th Chinese Control Conference, CCC 2011
Pages	3660-3663
Number of pages	4
State	Published - 2011
Event	30th Chinese Control Conference, CCC 2011 - Yantai, China Duration: 22 Jul 2011 → 24 Jul 2011

Publication series

Name	Proceedings of the 30th Chinese Control Conference, CCC 2011

Conference

Conference	30th Chinese Control Conference, CCC 2011
Country/Territory	China
City	Yantai
Period	22/07/11 → 24/07/11

Keywords

Autonomous Control
FCC
Flight Control
Semi-physical Simulation
Stability Augmentation

Cite this

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title = "Design of multi-mode flight control system for unmanned helicopter",

abstract = "Based on the special requirements of flight control and navigation system of unmanned helicopter, this paper present the main framework of flight control system in a certain type of unmanned helicopter, proposed three flight control modes based on different design stages, gave the autonomous control algorithm and the smoothing method while switching between remote control mode and stability augmentation mode, ultimately proved the feasibility of flight control and navigation program through the semi-physical simulation test and flight test.",

keywords = "Autonomous Control, FCC, Flight Control, Semi-physical Simulation, Stability Augmentation",

author = "Hongzhe Xu and Jun Huang and Yaoming Zhou",

year = "2011",

language = "英语",

isbn = "9789881725592",

series = "Proceedings of the 30th Chinese Control Conference, CCC 2011",

pages = "3660--3663",

booktitle = "Proceedings of the 30th Chinese Control Conference, CCC 2011",

note = "30th Chinese Control Conference, CCC 2011 ; Conference date: 22-07-2011 Through 24-07-2011",

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TY - GEN

T1 - Design of multi-mode flight control system for unmanned helicopter

AU - Xu, Hongzhe

AU - Huang, Jun

AU - Zhou, Yaoming

PY - 2011

Y1 - 2011

N2 - Based on the special requirements of flight control and navigation system of unmanned helicopter, this paper present the main framework of flight control system in a certain type of unmanned helicopter, proposed three flight control modes based on different design stages, gave the autonomous control algorithm and the smoothing method while switching between remote control mode and stability augmentation mode, ultimately proved the feasibility of flight control and navigation program through the semi-physical simulation test and flight test.

AB - Based on the special requirements of flight control and navigation system of unmanned helicopter, this paper present the main framework of flight control system in a certain type of unmanned helicopter, proposed three flight control modes based on different design stages, gave the autonomous control algorithm and the smoothing method while switching between remote control mode and stability augmentation mode, ultimately proved the feasibility of flight control and navigation program through the semi-physical simulation test and flight test.

KW - Autonomous Control

KW - FCC

KW - Flight Control

KW - Semi-physical Simulation

KW - Stability Augmentation

UR - https://www.scopus.com/pages/publications/80053066587

M3 - 会议稿件

AN - SCOPUS:80053066587

SN - 9789881725592

T3 - Proceedings of the 30th Chinese Control Conference, CCC 2011

SP - 3660

EP - 3663

BT - Proceedings of the 30th Chinese Control Conference, CCC 2011

T2 - 30th Chinese Control Conference, CCC 2011

Y2 - 22 July 2011 through 24 July 2011

ER -

Design of multi-mode flight control system for unmanned helicopter

Abstract

Publication series

Conference

Keywords

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Cite this