Altitude control using limited pole placement on coaxial-helicopter

Yasunori Sugawara, Akira Shimada

Research output: Chapter in Book/Report/Conference proceedingConference contribution

1 Citation (Scopus)

Abstract

This paper introduces an altitude control technique on coaxial-helicopter. Unmanned aerial vehicle (UAV) has been widely used with high performance computer (HPC) so far. Generally, advanced mathematics is used for flight control of the UAV on the HPC. However. the HPC has several problems, such as increase of cost and processing delays in calculation. We present a technique that performs the same control performance by using a low performance computer. In order to implement this technique, the limited pole placement (LPP) control is used for a prototype of electrical motor driven helicopter. Then, it is able to find out the critical efficiency of the control system considering time delay. Finally, this paper presents the good validation results by the experiment of the altitude control of the helicopter.

Original languageEnglish
Title of host publicationInternational Workshop on Advanced Motion Control, AMC
PublisherInstitute of Electrical and Electronics Engineers Inc.
Pages506-511
Number of pages6
ISBN (Print)9781479923243
DOIs
Publication statusPublished - 2014
Event2014 13th IEEE International Workshop on Advanced Motion Control, AMC 2014 - Yokohama
Duration: 2014 Mar 142014 Mar 16

Other

Other2014 13th IEEE International Workshop on Advanced Motion Control, AMC 2014
CityYokohama
Period14/3/1414/3/16

Fingerprint

Altitude control
Helicopters
Poles
Unmanned aerial vehicles (UAV)
Time delay
Control systems
Processing
Costs
Experiments

ASJC Scopus subject areas

  • Control and Systems Engineering
  • Electrical and Electronic Engineering
  • Computer Science Applications
  • Modelling and Simulation

Cite this

Sugawara, Y., & Shimada, A. (2014). Altitude control using limited pole placement on coaxial-helicopter. In International Workshop on Advanced Motion Control, AMC (pp. 506-511). [6823333] Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/AMC.2014.6823333

Altitude control using limited pole placement on coaxial-helicopter. / Sugawara, Yasunori; Shimada, Akira.

International Workshop on Advanced Motion Control, AMC. Institute of Electrical and Electronics Engineers Inc., 2014. p. 506-511 6823333.

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Sugawara, Y & Shimada, A 2014, Altitude control using limited pole placement on coaxial-helicopter. in International Workshop on Advanced Motion Control, AMC., 6823333, Institute of Electrical and Electronics Engineers Inc., pp. 506-511, 2014 13th IEEE International Workshop on Advanced Motion Control, AMC 2014, Yokohama, 14/3/14. https://doi.org/10.1109/AMC.2014.6823333
Sugawara Y, Shimada A. Altitude control using limited pole placement on coaxial-helicopter. In International Workshop on Advanced Motion Control, AMC. Institute of Electrical and Electronics Engineers Inc. 2014. p. 506-511. 6823333 https://doi.org/10.1109/AMC.2014.6823333
Sugawara, Yasunori ; Shimada, Akira. / Altitude control using limited pole placement on coaxial-helicopter. International Workshop on Advanced Motion Control, AMC. Institute of Electrical and Electronics Engineers Inc., 2014. pp. 506-511
@inproceedings{7af3dca123594130adf26141968e25be,
title = "Altitude control using limited pole placement on coaxial-helicopter",
abstract = "This paper introduces an altitude control technique on coaxial-helicopter. Unmanned aerial vehicle (UAV) has been widely used with high performance computer (HPC) so far. Generally, advanced mathematics is used for flight control of the UAV on the HPC. However. the HPC has several problems, such as increase of cost and processing delays in calculation. We present a technique that performs the same control performance by using a low performance computer. In order to implement this technique, the limited pole placement (LPP) control is used for a prototype of electrical motor driven helicopter. Then, it is able to find out the critical efficiency of the control system considering time delay. Finally, this paper presents the good validation results by the experiment of the altitude control of the helicopter.",
author = "Yasunori Sugawara and Akira Shimada",
year = "2014",
doi = "10.1109/AMC.2014.6823333",
language = "English",
isbn = "9781479923243",
pages = "506--511",
booktitle = "International Workshop on Advanced Motion Control, AMC",
publisher = "Institute of Electrical and Electronics Engineers Inc.",

}

TY - GEN

T1 - Altitude control using limited pole placement on coaxial-helicopter

AU - Sugawara, Yasunori

AU - Shimada, Akira

PY - 2014

Y1 - 2014

N2 - This paper introduces an altitude control technique on coaxial-helicopter. Unmanned aerial vehicle (UAV) has been widely used with high performance computer (HPC) so far. Generally, advanced mathematics is used for flight control of the UAV on the HPC. However. the HPC has several problems, such as increase of cost and processing delays in calculation. We present a technique that performs the same control performance by using a low performance computer. In order to implement this technique, the limited pole placement (LPP) control is used for a prototype of electrical motor driven helicopter. Then, it is able to find out the critical efficiency of the control system considering time delay. Finally, this paper presents the good validation results by the experiment of the altitude control of the helicopter.

AB - This paper introduces an altitude control technique on coaxial-helicopter. Unmanned aerial vehicle (UAV) has been widely used with high performance computer (HPC) so far. Generally, advanced mathematics is used for flight control of the UAV on the HPC. However. the HPC has several problems, such as increase of cost and processing delays in calculation. We present a technique that performs the same control performance by using a low performance computer. In order to implement this technique, the limited pole placement (LPP) control is used for a prototype of electrical motor driven helicopter. Then, it is able to find out the critical efficiency of the control system considering time delay. Finally, this paper presents the good validation results by the experiment of the altitude control of the helicopter.

UR - http://www.scopus.com/inward/record.url?scp=84903124863&partnerID=8YFLogxK

UR - http://www.scopus.com/inward/citedby.url?scp=84903124863&partnerID=8YFLogxK

U2 - 10.1109/AMC.2014.6823333

DO - 10.1109/AMC.2014.6823333

M3 - Conference contribution

AN - SCOPUS:84903124863

SN - 9781479923243

SP - 506

EP - 511

BT - International Workshop on Advanced Motion Control, AMC

PB - Institute of Electrical and Electronics Engineers Inc.

ER -