Relative Controllability Evaluation of Mass-Actuated Airplane

被引:10
作者
Erturk, Sukru Akif [1 ]
Dogan, Atilla [1 ]
机构
[1] Univ Texas Arlington, Mech & Aerosp Engn, Arlington, TX 76019 USA
关键词
MODAL CONTROLLABILITY; CONTROL-SYSTEM; OBSERVABILITY; PLACEMENT; OPTIMIZATION;
D O I
10.2514/1.G002858
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
引用
收藏
页码:384 / 393
页数:10
相关论文
共 55 条
[1]  
Ahn Y. K., 2012, THESIS
[2]   Optimal actuator/sensor placement for control of combustion instabilities [J].
Al-Masoud, N ;
Singh, T .
JOURNAL OF PROPULSION AND POWER, 2003, 19 (01) :148-151
[3]   Realistic determination of the optimal size and location of piezoelectric actuator/sensors [J].
Aldraihem, OJ ;
Singh, T ;
Wetherhold, RC .
PROCEEDINGS OF THE 1997 IEEE INTERNATIONAL CONFERENCE ON CONTROL APPLICATIONS, 1997, :435-440
[4]  
Balaram J, 2005, Proceedings of the ASME International Design Engineering Technical Conferences and Computers and Information in Engineering Conference, Vol 6, Pts A-C, P63
[5]  
Beyer E. W., 2009, THESIS
[6]   Composite Control Strategy of Stratospheric Airships with Moving Masses [J].
Chen, L. ;
Zhou, G. ;
Yan, X. J. ;
Duan, D. P. .
JOURNAL OF AIRCRAFT, 2012, 49 (03) :794-801
[7]   Modal controllability and observability of bladed disks and their dependency on the angular velocity [J].
Christensen, RH ;
Santos, IMF .
JOURNAL OF VIBRATION AND CONTROL, 2005, 11 (06) :801-828
[8]  
Collard D., 1991, SAE(Society of Automotive Engineers) Transactions, V100, P2620
[9]   Controllability Analysis for Multirotor Helicopter Rotor Degradation and Failure [J].
Du, Guang-Xun ;
Quan, Quan ;
Yang, Binxian ;
Cai, Kai-Yuan .
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2015, 38 (05) :978-984
[10]  
Erturk S. A., 2017, AIAA ATM FLIGHT MECH, DOI DOI 10.2514/6.2017-1636