Результаты исследований: Публикации в книгах, отчётах, сборниках, трудах конференций › статья в сборнике материалов конференции › научная › Рецензирование
On the choosing problem of PID controller parameters for a quadrocopter. / Baranov, Oleg V.; Smirnov, Nikolay V.; Smirnova, Tatiana E.
2017 Constructive Nonsmooth Analysis and Related Topics (Dedicated to the Memory of V.F. Demyanov), CNSA 2017 - Proceedings. ред. / L. N. Polyakova. Institute of Electrical and Electronics Engineers Inc., 2017. 7973934.Результаты исследований: Публикации в книгах, отчётах, сборниках, трудах конференций › статья в сборнике материалов конференции › научная › Рецензирование
}
TY - GEN
T1 - On the choosing problem of PID controller parameters for a quadrocopter
AU - Baranov, Oleg V.
AU - Smirnov, Nikolay V.
AU - Smirnova, Tatiana E.
PY - 2017/7/10
Y1 - 2017/7/10
N2 - At present, quadrocopters are widely used. Therefore, the problems of controlling quadrocopters in real operating conditions, including emergency modes, are of particular interest. This is due to various weather conditions, restrictions on the landing place (the presence of water surface and other obstacles). So the stabilization problem is considered in this paper. To stabilize the apparatus in three planes, it is proposed to use three PID controllers. The parameters choice in this case has features related to the basic technical and geometric characteristics of the quadrocopter. The modeling results of the real time stabilization are presented. Some recommendations of simplification of the empirical choosing of PID controller parameters depending on the possibilities of the flight controller are given.
AB - At present, quadrocopters are widely used. Therefore, the problems of controlling quadrocopters in real operating conditions, including emergency modes, are of particular interest. This is due to various weather conditions, restrictions on the landing place (the presence of water surface and other obstacles). So the stabilization problem is considered in this paper. To stabilize the apparatus in three planes, it is proposed to use three PID controllers. The parameters choice in this case has features related to the basic technical and geometric characteristics of the quadrocopter. The modeling results of the real time stabilization are presented. Some recommendations of simplification of the empirical choosing of PID controller parameters depending on the possibilities of the flight controller are given.
UR - http://www.scopus.com/inward/record.url?scp=85027442739&partnerID=8YFLogxK
UR - http://proxy.library.spbu.ru:2104/full_record.do?product=WOS&search_mode=DaisyOneClickSearch&qid=3&SID=D4zk9sd79amcsNyxcbH&page=1&doc=2
U2 - 10.1109/CNSA.2017.7973934
DO - 10.1109/CNSA.2017.7973934
M3 - Conference contribution
AN - SCOPUS:85027442739
BT - 2017 Constructive Nonsmooth Analysis and Related Topics (Dedicated to the Memory of V.F. Demyanov), CNSA 2017 - Proceedings
A2 - Polyakova, L. N.
PB - Institute of Electrical and Electronics Engineers Inc.
T2 - 2017 Constructive Nonsmooth Analysis and Related Topics
Y2 - 22 May 2017 through 27 May 2017
ER -
ID: 36124494