Observer-based H-infinity Tracking Control Design for A Linearized Hypersonic Vehicle Model with External Disturbance
被引:0
作者:
Gao, Zhifeng
论文数: 0引用数: 0
h-index: 0
机构:
Nanjing Univ Posts & Telecommun, Coll Automat, Nanjing 210046, Jiangsu, Peoples R ChinaNanjing Univ Posts & Telecommun, Coll Automat, Nanjing 210046, Jiangsu, Peoples R China
Gao, Zhifeng
[1
]
Cao, Teng
论文数: 0引用数: 0
h-index: 0
机构:
Nanjing Univ Posts & Telecommun, Coll Automat, Nanjing 210046, Jiangsu, Peoples R ChinaNanjing Univ Posts & Telecommun, Coll Automat, Nanjing 210046, Jiangsu, Peoples R China
Cao, Teng
[1
]
Lin, Jinxing
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h-index: 0
机构:
Nanjing Univ Posts & Telecommun, Coll Automat, Nanjing 210046, Jiangsu, Peoples R ChinaNanjing Univ Posts & Telecommun, Coll Automat, Nanjing 210046, Jiangsu, Peoples R China
Lin, Jinxing
[1
]
Qian, Moshu
论文数: 0引用数: 0
h-index: 0
机构:
Nanjing Univ Aeronaut & Astronaut, Res Inst UAV, Nanjing 210016, Jiangsu, Peoples R ChinaNanjing Univ Posts & Telecommun, Coll Automat, Nanjing 210046, Jiangsu, Peoples R China
Qian, Moshu
[2
]
机构:
[1] Nanjing Univ Posts & Telecommun, Coll Automat, Nanjing 210046, Jiangsu, Peoples R China
[2] Nanjing Univ Aeronaut & Astronaut, Res Inst UAV, Nanjing 210016, Jiangsu, Peoples R China
来源:
2014 IEEE CHINESE GUIDANCE, NAVIGATION AND CONTROL CONFERENCE (CGNCC)
|
2014年
关键词:
SWITCHING CONTROL;
FLIGHT VEHICLE;
D O I:
暂无
中图分类号:
TM [电工技术];
TN [电子技术、通信技术];
学科分类号:
0808 ;
0809 ;
摘要:
In this study, the H-infinity tracking control problem of a linearized hypersonic vehicle model with the bounded external disturbance is investigated. Firstly, the nonlinear longitudinal dynamics of hypersonic vehicle is linearized as a linear time-invariant system with the bounded external disturbance, a reference model is introduced for the aim of tracking control. And then an observer-based output feedback tracking controller design approach is proposed by using the linear matrix inequalities (LMIs) technique. The asymptotical stability of the closed-loop system is analyzed in the framework of Lyapunov method. Finally, the simulation results are given to illustrate the applicability of the developed control approach.