Comparison of frequency responses with PID and two degree-of-freedom PID control for underactuated flying object

Syouya Mizokami, Kohei Yoshikawa, Akira Yanou, Mamoru Minami, Takayuki Matsuno

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

Abstract

Flying object used in our research is an experimental device like a helicopter. Helicopter, which has a special characteristics such as hovering, vertical ascent and vertical dive. Therefore, it is widely used at the time of disaster. For example, manned helicopter is used for rescue work, emergency transport and fire fighting. On the contrary, unmanned helicopter is used to get precious information in a danger area for human. But there are problems that the structure is complicated, it has a high nonlinearity. And it is difficult to keep the attitude, because it is influenced by wind in flight. An experimental device in our research has an underactuated system having 2-input and 3-output that has number of input less than number of output. So, this system is able to reduce cost, but to keep the posture is difficult. Therefore, in our research, a stabilization method called two degree-of-freedom PID control has been proposed. It is the system having three degree-of-freedom. Although the effectiveness has been confirmed through the simulation and experimental results in time-domain, the characteristics of the proposed method was just explored by the result of output for step-type reference signal. Therefore, this paper confirms the effectiveness of the proposed method through the simulation and experimental result in frequency-domain in order to check the characteristics of the proposed method.

Original languageEnglish
Title of host publicationProceedings of the SICE Annual Conference
Pages1192-1196
Number of pages5
Publication statusPublished - 2013
Event2013 52nd Annual Conference of the Society of Instrument and Control Engineers of Japan, SICE 2013 - Nagoya, Japan
Duration: Sep 14 2013Sep 17 2013

Other

Other2013 52nd Annual Conference of the Society of Instrument and Control Engineers of Japan, SICE 2013
CountryJapan
CityNagoya
Period9/14/139/17/13

Fingerprint

Three term control systems
Helicopters
Frequency response
Disasters
Fires
Stabilization
Costs

Keywords

  • Frequency response
  • Two degree-of-freedom PID
  • Underactuated flying object

ASJC Scopus subject areas

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

Cite this

Mizokami, S., Yoshikawa, K., Yanou, A., Minami, M., & Matsuno, T. (2013). Comparison of frequency responses with PID and two degree-of-freedom PID control for underactuated flying object. In Proceedings of the SICE Annual Conference (pp. 1192-1196)

Comparison of frequency responses with PID and two degree-of-freedom PID control for underactuated flying object. / Mizokami, Syouya; Yoshikawa, Kohei; Yanou, Akira; Minami, Mamoru; Matsuno, Takayuki.

Proceedings of the SICE Annual Conference. 2013. p. 1192-1196.

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

Mizokami, S, Yoshikawa, K, Yanou, A, Minami, M & Matsuno, T 2013, Comparison of frequency responses with PID and two degree-of-freedom PID control for underactuated flying object. in Proceedings of the SICE Annual Conference. pp. 1192-1196, 2013 52nd Annual Conference of the Society of Instrument and Control Engineers of Japan, SICE 2013, Nagoya, Japan, 9/14/13.
Mizokami S, Yoshikawa K, Yanou A, Minami M, Matsuno T. Comparison of frequency responses with PID and two degree-of-freedom PID control for underactuated flying object. In Proceedings of the SICE Annual Conference. 2013. p. 1192-1196
Mizokami, Syouya ; Yoshikawa, Kohei ; Yanou, Akira ; Minami, Mamoru ; Matsuno, Takayuki. / Comparison of frequency responses with PID and two degree-of-freedom PID control for underactuated flying object. Proceedings of the SICE Annual Conference. 2013. pp. 1192-1196
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